DAHER AIRCRAFT, SAS TBM 700: certification basis
Basis entries as written on the TCDS
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14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-34 and Sections 23.783, 23.811 and 23.807 of Amendments 36
Applies to: Airplanes not equipped with modification No. MOD 70-139-00 (see note 6)
Includes 14 CFR 23 through 23-34 · current is 23-63, 27 revisions later
Includes 14 CFR 23 §23.783, §23.807, §23.811 through 23-36 · current is 23-63, 25 revisions later
Expands to 333 provision links ! 2 text missing · shown below
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14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-17.
Applies to: Airplanes not equipped with modification No. MOD 70-139-00 (see note 6)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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Special Federal Aviation Regulation Number 27, effective February 1, 1974 including Amendments 27-1 through 27-6.
Applies to: Airplanes not equipped with modification No. MOD 70-139-00 (see note 6)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-34, Sections 23.783, 23.811 and 23.807 of Amendments 36 and Sections 23.49, 23.561, 23.562 and 23.785 of Amendment 44.
Applies to: Airplanes equipped with modification No. MOD 70-139-00 (see note 6)
Includes 14 CFR 23 through 23-34 · current is 23-63, 27 revisions later
Includes 14 CFR 23 §23.783, §23.807, §23.811 through 23-36 · current is 23-63, 25 revisions later
Includes 14 CFR 23 §23.49, §23.561, §23.562, §23.785 through 23-44 · current is 23-63, 17 revisions later
Expands to 334 provision links ! 2 text missing · Show the expansion
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14 CFR Part 34 effective September 10,1990, including Amendments 34-1 through Amendment 34-3.
Applies to: Airplanes equipped with modification No. MOD 70-139-00 (see note 6)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-22.
Applies to: Airplanes equipped with modification No. MOD 70-139-00 (see note 6)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-34, Section 23.1301 of Amendment 23-20, Sections 23.783, 23.811 and 23.807 of Amendments 36, Sections 23.1322 and 23.1331 of Amendment 43, Sections 23.49, 23.561, 23.562 and 23.785 of Amendment 44, Sections 23.1309, 23.1311 23.1321, 23.1323, 23.1353, 23.1365 and 23.1431 of Amendment 49 and Section 23.1308 of Amendment 57.
Applies to: Airplanes (s/n 434-999, except 687) equipped with modification No. MOD 70-0211-57 (“Fuel tanks extension”), modification No. MOD 70-0176-00 (“Garmin G1000”), and optional modification No. MOD 70-0226-00 (“SVS” option to G1000) (see notes 8, 9, 10, 11, 12)
Includes 14 CFR 23 through 23-34 · current is 23-63, 27 revisions later
Includes 14 CFR 23 §23.1301 through 23-20 · current is 23-63, 41 revisions later
Includes 14 CFR 23 §23.783, §23.807, §23.811 through 23-36 · current is 23-63, 25 revisions later
Includes 14 CFR 23 §23.1322, §23.1331 through 23-43 · current is 23-63, 18 revisions later
Includes 14 CFR 23 §23.49, §23.561, §23.562, §23.785 through 23-44 · current is 23-63, 17 revisions later
Includes 14 CFR 23 §23.1309, §23.1311, §23.1321, §23.1323, §23.1353, §23.1365, §23.1431 through 23-49 · current is 23-63, 12 revisions later
Includes 14 CFR 23 §23.1308 through 23-57 · current is 23-63, 5 revisions later
Expands to 336 provision links ! 2 text missing · Show the expansion
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14 CFR Part 34 effective September 10, 1990, including Amendments 34-1 through Amendment 34-3.
Applies to: Airplanes (s/n 434-999, except 687) equipped with modification No. MOD 70-0211-57 (“Fuel tanks extension”), modification No. MOD 70-0176-00 (“Garmin G1000”), and optional modification No. MOD 70-0226-00 (“SVS” option to G1000) (see notes 8, 9, 10, 11, 12)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-22.
Applies to: Airplanes (s/n 434-999, except 687) equipped with modification No. MOD 70-0211-57 (“Fuel tanks extension”), modification No. MOD 70-0176-00 (“Garmin G1000”), and optional modification No. MOD 70-0226-00 (“SVS” option to G1000) (see notes 8, 9, 10, 11, 12)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-34, Section 23.1301 of Amendment 23-20, Sections 23.783, 23.811 and 23.807 of Amendments 36, Sections 23.1322 and 23.1331 of Amendment 43, Sections 23.49, 23.561, 23.562 and 23.785 of Amendment 44, Sections 23.1309, 23.1311 23.1321, 23.1323, 23.1353, 23.1365 and 23.1431 of Amendment 49, Section 23.207 of Amendment 50, Section 23.1308 of Amendment 57 and Section 23.1306 of Amendment 61. (Note: Airplanes equipped with optional modification No. MOD70- 0423-34 “Lift transducer and AOA” also include Section 23.207 of Amendment 50. Airplanes equipped with optional modification No. MOD70-0388- 25 “AMSAFE Airbag Seatbelt on Pilot and Co-Pilot Seats” also include FAA Special Conditions No. 23-276-SC.)
Applies to: Airplanes (s/n 687, 1000-1105) equipped with modification MOD 70-0176-00 (“Garmin G1000”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70- 0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), optional modification No. MOD70-407-00 (“Aural alerts evolution and V15 Software for G1000 Integrated Flight Deck on TBM850/900“) and optional modification No. MOD70- 0407-00 Ed 2 Version C (“ESP and USP option to G1000”) (see notes 18, 19, 20, 21, 22 and 23): or Airplanes (s/n 1170-9999) equipped with modification MOD 70-0176-00 (“Garmin G1000”) and optional modification MOD70-0539-00 (“Garmin G1000 Nxi”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70- 0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), optional modification No. MOD70-407-00 (“Aural alerts evolution and V15 Software for G1000 Integrated Flight Deck on TBM850/900“) and optional modification No. MOD70- 0407-00 Ed 2 Version C (“ESP and USP option to G1000”) (see notes 18, 19, 20, 21, 22, 23, 24 and 25)
Includes 14 CFR 23 through 23-34 · current is 23-63, 27 revisions later
Includes 14 CFR 23 §23.1301 through 23-20 · current is 23-63, 41 revisions later
Includes 14 CFR 23 §23.783, §23.807, §23.811 through 23-36 · current is 23-63, 25 revisions later
Includes 14 CFR 23 §23.1322, §23.1331 through 23-43 · current is 23-63, 18 revisions later
Includes 14 CFR 23 §23.49, §23.561, §23.562, §23.785 through 23-44 · current is 23-63, 17 revisions later
Includes 14 CFR 23 §23.1309, §23.1311, §23.1321, §23.1323, §23.1353, §23.1365, §23.1431 through 23-49 · current is 23-63, 12 revisions later
Includes 14 CFR 23 §23.207 through 23-50 · current is 23-63, 11 revisions later
Includes 14 CFR 23 §23.1308 through 23-57 · current is 23-63, 5 revisions later
Includes 14 CFR 23 §23.1306 through 23-61 · current is 23-63, 2 revisions later
Includes 14 CFR 23 §23.207 through 23-50 · current is 23-63, 11 revisions later
Expands to 337 provision links ! 2 text missing · Show the expansion
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14 CFR Part 34 effective September 10,1990, including Amendments 34-1 through Amendment 34-3.
Applies to: Airplanes (s/n 687, 1000-1105) equipped with modification MOD 70-0176-00 (“Garmin G1000”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70- 0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), optional modification No. MOD70-407-00 (“Aural alerts evolution and V15 Software for G1000 Integrated Flight Deck on TBM850/900“) and optional modification No. MOD70- 0407-00 Ed 2 Version C (“ESP and USP option to G1000”) (see notes 18, 19, 20, 21, 22 and 23): or Airplanes (s/n 1170-9999) equipped with modification MOD 70-0176-00 (“Garmin G1000”) and optional modification MOD70-0539-00 (“Garmin G1000 Nxi”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70- 0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), optional modification No. MOD70-407-00 (“Aural alerts evolution and V15 Software for G1000 Integrated Flight Deck on TBM850/900“) and optional modification No. MOD70- 0407-00 Ed 2 Version C (“ESP and USP option to G1000”) (see notes 18, 19, 20, 21, 22, 23, 24 and 25)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-28.
Applies to: Airplanes (s/n 687, 1000-1105) equipped with modification MOD 70-0176-00 (“Garmin G1000”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70- 0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), optional modification No. MOD70-407-00 (“Aural alerts evolution and V15 Software for G1000 Integrated Flight Deck on TBM850/900“) and optional modification No. MOD70- 0407-00 Ed 2 Version C (“ESP and USP option to G1000”) (see notes 18, 19, 20, 21, 22 and 23): or Airplanes (s/n 1170-9999) equipped with modification MOD 70-0176-00 (“Garmin G1000”) and optional modification MOD70-0539-00 (“Garmin G1000 Nxi”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70- 0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), optional modification No. MOD70-407-00 (“Aural alerts evolution and V15 Software for G1000 Integrated Flight Deck on TBM850/900“) and optional modification No. MOD70- 0407-00 Ed 2 Version C (“ESP and USP option to G1000”) (see notes 18, 19, 20, 21, 22, 23, 24 and 25)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-34, Section 23.1301 of Amendment 23-20, Sections 23.783, 23.811 and 23.807 of Amendments 36, Sections 23.1322 and 23.1331 of Amendment 43, Sections 23.49, 23.561, 23.562 and 23.785 of Amendment 44, Sections 23.1309, 23.1311 23.1321, 23.1323, 23.1353, 23.1365 and 23.1431 of Amendment 49, Section 23.207 of Amendment 50, Section 23.1308 of Amendment 57 and Section 23.1306 of Amendment 61. (Note: Airplanes equipped with optional modification No. MOD70- 0423-34 “Lift transducer and AOA” also include Section 23.207 of Amendment 50. Section 1308 of Amendment57 and Section 23.1306 of Amendment 61.
Applies to: Airplanes (s/n 1111-1215) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000), modification No. MOD 70- 0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70- 0357-71 (“Take-off and landing operations at 850SHP”) and optional modification No MOD70-0345-61 (“New five-blade propeller”) (see notes 18, 19, 20, 21, 22 and 23): or Airplanes (s/n 1216-9999) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000) and optional modification No. MOD70-0549-00 (“Garmin G3000 2018”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take- off and landing operations at 850SHP”) and optional modification No MOD70-0345-61 (“New five-blade propeller”) (see notes 18, 19, 20, 21, 22, 23, 24 and 26): or Airplanes (s/n 1272, 1275-9999) equipped with optional modification No. MOD70-0476- 00 (“Garmin G3000” including ESP and USP option to G3000), optional modification No. MOD70-0549-00 (“Garmin G3000 2018”) and optional modification No. MOD70-0649- 00 (“G3000 system Software V21.25”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take- off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), modification No. MOD70-0550-00 (“Auto-throttle”), modification No. MOD70-0619-11 (“Modification of cabin interior markings”) and optional modification No. MOD70-0632-34 (“Magnetometer MD032 integration”) (see notes 18, 19, 20, 21, 22, 23, 24, 31 and 32): or Airplanes (s/n 1333-9999) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000), optional modification No. MOD70-0549-00 (“Garmin G3000 2018”) and optional modification No. MOD70-0649- 00 Version E (G3000 system new Software SR 5.1.8) and optional modification No. MOD70-0650-34 (“Emergency Autoland/HomeSafe system”), modification No. MOD 70- 0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70- 0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), modification No. MOD70-0550-00 (“Auto-throttle”), modification No. MOD70-0619-11 (“Modification of cabin interior markings”) and optional modification No. MOD70-0632-34 (“Magnetometer MD032 integration”) (see notes 18, 19, 20, 21, 22, 23, 24, 31, 32 and 33)
Includes 14 CFR 23 through 23-34 · current is 23-63, 27 revisions later
Includes 14 CFR 23 §23.1301 through 23-20 · current is 23-63, 41 revisions later
Includes 14 CFR 23 §23.783, §23.807, §23.811 through 23-36 · current is 23-63, 25 revisions later
Includes 14 CFR 23 §23.1322, §23.1331 through 23-43 · current is 23-63, 18 revisions later
Includes 14 CFR 23 §23.49, §23.561, §23.562, §23.785 through 23-44 · current is 23-63, 17 revisions later
Includes 14 CFR 23 §23.1309, §23.1311, §23.1321, §23.1323, §23.1353, §23.1365, §23.1431 through 23-49 · current is 23-63, 12 revisions later
Includes 14 CFR 23 §23.207 through 23-50 · current is 23-63, 11 revisions later
Includes 14 CFR 23 §23.1308 through 23-57 · current is 23-63, 5 revisions later
Includes 14 CFR 23 §23.1306 through 23-61 · current is 23-63, 2 revisions later
Includes 14 CFR 23 §23.207 through 23-50 · current is 23-63, 11 revisions later
Includes 14 CFR 23 §23.1306 through 23-61 · current is 23-63, 2 revisions later
Expands to 337 provision links ! 2 text missing · Show the expansion
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14 CFR Part 34 effective September 10,1990, including Amendments 34-1 through Amendment 34-3.
Applies to: Airplanes (s/n 1111-1215) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000), modification No. MOD 70- 0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70- 0357-71 (“Take-off and landing operations at 850SHP”) and optional modification No MOD70-0345-61 (“New five-blade propeller”) (see notes 18, 19, 20, 21, 22 and 23): or Airplanes (s/n 1216-9999) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000) and optional modification No. MOD70-0549-00 (“Garmin G3000 2018”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take- off and landing operations at 850SHP”) and optional modification No MOD70-0345-61 (“New five-blade propeller”) (see notes 18, 19, 20, 21, 22, 23, 24 and 26): or Airplanes (s/n 1272, 1275-9999) equipped with optional modification No. MOD70-0476- 00 (“Garmin G3000” including ESP and USP option to G3000), optional modification No. MOD70-0549-00 (“Garmin G3000 2018”) and optional modification No. MOD70-0649- 00 (“G3000 system Software V21.25”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take- off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), modification No. MOD70-0550-00 (“Auto-throttle”), modification No. MOD70-0619-11 (“Modification of cabin interior markings”) and optional modification No. MOD70-0632-34 (“Magnetometer MD032 integration”) (see notes 18, 19, 20, 21, 22, 23, 24, 31 and 32): or Airplanes (s/n 1333-9999) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000), optional modification No. MOD70-0549-00 (“Garmin G3000 2018”) and optional modification No. MOD70-0649- 00 Version E (G3000 system new Software SR 5.1.8) and optional modification No. MOD70-0650-34 (“Emergency Autoland/HomeSafe system”), modification No. MOD 70- 0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70- 0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), modification No. MOD70-0550-00 (“Auto-throttle”), modification No. MOD70-0619-11 (“Modification of cabin interior markings”) and optional modification No. MOD70-0632-34 (“Magnetometer MD032 integration”) (see notes 18, 19, 20, 21, 22, 23, 24, 31, 32 and 33)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-28.
Applies to: Airplanes (s/n 1111-1215) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000), modification No. MOD 70- 0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70- 0357-71 (“Take-off and landing operations at 850SHP”) and optional modification No MOD70-0345-61 (“New five-blade propeller”) (see notes 18, 19, 20, 21, 22 and 23): or Airplanes (s/n 1216-9999) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000) and optional modification No. MOD70-0549-00 (“Garmin G3000 2018”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take- off and landing operations at 850SHP”) and optional modification No MOD70-0345-61 (“New five-blade propeller”) (see notes 18, 19, 20, 21, 22, 23, 24 and 26): or Airplanes (s/n 1272, 1275-9999) equipped with optional modification No. MOD70-0476- 00 (“Garmin G3000” including ESP and USP option to G3000), optional modification No. MOD70-0549-00 (“Garmin G3000 2018”) and optional modification No. MOD70-0649- 00 (“G3000 system Software V21.25”), modification No. MOD 70-0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70-0357-71 (“Take- off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), modification No. MOD70-0550-00 (“Auto-throttle”), modification No. MOD70-0619-11 (“Modification of cabin interior markings”) and optional modification No. MOD70-0632-34 (“Magnetometer MD032 integration”) (see notes 18, 19, 20, 21, 22, 23, 24, 31 and 32): or Airplanes (s/n 1333-9999) equipped with optional modification No. MOD70-0476-00 (“Garmin G3000” including ESP and USP option to G3000), optional modification No. MOD70-0549-00 (“Garmin G3000 2018”) and optional modification No. MOD70-0649- 00 Version E (G3000 system new Software SR 5.1.8) and optional modification No. MOD70-0650-34 (“Emergency Autoland/HomeSafe system”), modification No. MOD 70- 0234-24 (“New electrical generation and primary distribution”), MOD70-0322-00 (“Aerodynamic efficiency improvement”), MOD70-0323-71 (“Propulsion efficiency improvement”), MOD70-0324-00 (“Human Machine Interface improvement”), MOD70- 0357-71 (“Take-off and landing operations at 850SHP”), optional modification No MOD70-0345-61 (“New five-blade propeller”), modification No. MOD70-0550-00 (“Auto-throttle”), modification No. MOD70-0619-11 (“Modification of cabin interior markings”) and optional modification No. MOD70-0632-34 (“Magnetometer MD032 integration”) (see notes 18, 19, 20, 21, 22, 23, 24, 31, 32 and 33)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-34, Section 23.1301 of Amendment 23-20, Sections 23.783, 23.811 and 23.807 of Amendments 36, Sections 23.1322 and 23.1331 of Amendment 43, Sections 23.49, 23.561, 23.562 and 23.785 of Amendment 44, Sections 23.1309, 23.1311 23.1321, 23.1323, 23.1353, 23.1365 and 23.1431 of Amendment 49, Section 23.207 of Amendment 50, Section 23.1308 of Amendment 57 and Section 23.1306 of Amendment 61. (Note: Airplanes equipped with optional modification No. MOD70- 0423-34 “Lift transducer and AOA” also include Section 23.207 of Amendment 50. Section 1308 of Amendment 57 and Section 23.1306 of Amendment 61.
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 34 effective September 10,1990, including Amendments 34-1 through Amendment 34-3.
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-28.
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23 at Amendment 23-64 sections 23.2005, 23.2010, 23.2105, 23.2115(a)(1)(2)(3)(b), 23.2120(a)(1)(2)(c), 23.2125, 23.2135, 23.2140, 23.2145, 23.2155, 23.2160, 23.2200, 23.2205, 23.2210, 23.2215, 23.2225, 23.2230, 23.2235, 23.2240(a)(b)(c)(1)(2), 23.2245, 23.2300, 23.2335, 23.2400(a)(b)(c)(1)(2)(3)(4)(e), 23.2405, 23.2410, 23.2415, 23.2420, 23.2425, 23.2500(a)(1)(2), 23.2505, 23.2510, 23.2515, 23.2520, 23.2525, 23.2600, 23.2605, 23.2610, 23.2615, 23.2620, Appendix A
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”); Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0621-76 (“Engine power increase, Engine control and e-Throttle”), modification No. MOD70-0665-61 (“Five blades Raptor Propeller”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 23, including Amendments 23-1 through Amendment 23-62. -Sections 23.201, 23.203, 23.207, 23.221
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”); Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0621-76 (“Engine power increase, Engine control and e-Throttle”), modification No. MOD70-0665-61 (“Five blades Raptor Propeller”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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14 CFR Part 34 effective September 10,1990, including Amendments 34-1 through Amendment 34-6.
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”); Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0621-76 (“Engine power increase, Engine control and e-Throttle”), modification No. MOD70-0665-61 (“Five blades Raptor Propeller”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through Amendment 36-31, Appendix G.
Applies to: Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0646-21 (“ENVIRO components based ECS”), modification No. MOD70-0753-00 (“Software Upgrade”), modification No. MOD70-0680-10 (“Weight and balance modification”); Airplanes (s/n 1408-9999) equipped with modifications No. MOD70-0621-76 (“Engine power increase, Engine control and e-Throttle”), modification No. MOD70-0665-61 (“Five blades Raptor Propeller”)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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ELOS
ELOS ACE-02-01: 14 CFR §23.807(a)(1), Emergency Exits; Refer to FAA letter dated October 7, 2001, applicable to cargo configured airplanes only (See Note 4.)
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ELOS
ELOS ACE-14-01: 14 CFR §23.777(d) Cockpit Controls Location and 14 CFR §23.781(b), Shape – Single Power Lever for TBM 700 dated December 12, 2013, applicable to aircraft equipped with MOD70-0324-00 (see note 21)
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ELOS
ELOS AT01004CE-A-P-2: 14 CFR §23.1305(e),(j, and (m), amendment 23-24, Part Time and Full Time Digital Only Powerplant Indications, applicable for aircraft equipped with MOD70-0550-00 (see note 31)
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ELOS
ELOS AT01078CE-A-S-2: 14 CFR part 23 §23.671, 23.697, 23.729, 23.777, 23.779, 23.991, 23.1141, 23.1189, 23.1301, 23.1303, 23.1305, 23.1309, 23.1311, 23.1321, 23.1322, 23.1337, 23.1555, Airplanes equipped with DAHER modification No. MOD70-0650-34 (“Emergency Autoland/HomeSafe System”) s/n 1272, 1275-9999
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ELOS
ELOS AT11910IB-A-23.1303:14 CFR 21.21(b)(1), 23.1301, 23.1303, 23.1309, 23.1311, 23.1321, 23.1459 Indications removal from Primary Flight Displays during ground phase on Model Daher TBM700N airplane Airplanes equipped with DAHER modification No. MOD70-0876-00
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◆ SPECIAL
Special Condition No. 23-276-SC Airbag seatbelt on Pilot and Co-Pilot Seats (See Note 24)
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◆ SPECIAL
Special Condition No. 23-296-SC Autothrust System effective August 30, 2019 (See Note 31)
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OTHER
Approved for flight into known icing.
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OTHER
Direction Générale de l’Aviation Civile (DGAC) originally type certified this aircraft under its type certificate number TC 181, and EASA Type Certificate Number EASA.A.010. The FAA validated this product under U.S. Type Certificate Number A60EU. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of France.
- Exemptions: none recorded.
Entry 1 expanded
General 14 CFR 23 3 sections
Flight 14 CFR 23 44 sections
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.21 | Proof of compliance. General | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.23 | Load distribution limits. General | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.25 | Weight limits. General | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.29 | Empty weight and corresponding center of gravity. General | 23-34 | 23-21 | 0 | ✓ Text available |
| §23.31 | Removable ballast. General | 23-34 | 23-13 | 0 | ✓ Text available |
| §23.33 | Propeller speed and pitch limits. General | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.45 | General. Performance | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.49 | Stalling speed. Performance | 23-34 | 23-21 | 3 | ✓ Text available |
| §23.51 | Takeoff speeds. Performance | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.53 | Takeoff performance. Performance | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.55 | Accelerate-stop distance. Performance | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.57 | Takeoff path. Performance | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.59 | Takeoff distance and takeoff run. Performance | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.61 | Takeoff flight path. Performance | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.65 | Climb: All engines operating. Performance | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.67 | Climb: One engine inoperative. Performance | 23-34 | 23-34 | 5 | ✓ Text available |
| §23.75 | Landing [distance.] Performance | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.77 | Balked landing. Performance | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.141 | Flight Characteristics | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.143 | Controllability and Maneuverability Controllability and Maneuverability | 23-34 | 23-17 | 2 | ✓ Text available |
| §23.145 | Longitudinal control. Controllability and Maneuverability | 23-34 | 23-17 | 2 | ✓ Text available |
| §23.147 | Directional and lateral control. Controllability and Maneuverability | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.149 | Minimum control speed. Controllability and Maneuverability | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.151 | Acrobatic maneuvers. Controllability and Maneuverability | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.153 | Control during landings. Controllability and Maneuverability | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.155 | Elevator control force in maneuvers. Controllability and Maneuverability | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.157 | Rate of roll. Controllability and Maneuverability | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.161 | Trim. Trim | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.171 | General. Stability | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.173 | Static longitudinal stability. Stability | 23-34 | 23-34 | 0 | ✓ Text available |
| §23.175 | Demonstration of static longitudinal stability. Stability | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.177 | Static directional and lateral stability. Stability | 23-34 | 23-21 | 3 | ✓ Text available |
| §23.181 | Dynamic stability. Stability | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.201 | Wings level stall. Stalls | 23-34 | 23-14 | 3 | ✓ Text available |
| §23.203 | Turning flight and accelerated turning stalls. Stalls | 23-34 | 23-14 | 3 | ✓ Text available |
| §23.205 | Critical engine inoperative stalls. Stalls | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.207 | Stall warning. Stalls | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.221 | Spinning. Spinning | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.231 | Longitudinal stability and control. Ground and Water Handling Characteristics | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.233 | Directional stability and control. Ground and Water Handling Characteristics | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.235 | Operation on unpaved surfaces. Ground and Water Handling Characteristics | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.239 | Spray characteristics. Ground and Water Handling Characteristics | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.251 | Vibration and buffeting. Miscellaneous Flight Requirements | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.253 | High speed characteristics. Miscellaneous Flight Requirements | 23-34 | 23-26 | 3 | ✓ Text available |
Structure 14 CFR 23 56 sections
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.301 | Loads. General | 23-34 | 23-28 | 2 | ✓ Text available |
| §23.305 | Strength and deformation. General | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.307 | Proof of structure. General | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.321 | General. Flight Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.331 | Symmetrical flight conditions. Flight Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.333 | Flight envelope. Flight Loads | 23-34 | 23-34 | 0 | ✓ Text available |
| §23.335 | Design airspeeds. Flight Loads | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.337 | Limit maneuvering load factors. Flight Loads | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.341 | Gust load factors. Flight Loads | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.345 | High lift devices. Flight Loads | 23-34 | 23-23 | 1 | ✓ Text available |
| §23.347 | Unsymmetrical flight conditions. Flight Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.349 | Rolling conditions. Flight Loads | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.351 | Yawing conditions. Flight Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.361 | Engine torque. Flight Loads | 23-34 | 23-26 | 1 | ✓ Text available |
| §23.363 | Side load on engine mount. Flight Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.365 | Pressurized cabin loads. Flight Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.367 | Unsymmetrical loads due to engine failure. Flight Loads | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.369 | Rear lift truss. Flight Loads | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.371 | Gyroscopic and aerodynamic loads. Flight Loads | 23-34 | 23-26 | 2 | ✓ Text available |
| §23.373 | Speed control devices. Flight Loads | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.391 | Control surface loads. Control Surface and System Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.395 | Control system [loads.] Control Surface and System Loads | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.397 | Limit control forces and torques. Control Surface and System Loads | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.399 | Dual control system. Control Surface and System Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.405 | Secondary control system. Control Surface and System Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.407 | Trim tab effects. Control Surface and System Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.409 | Tabs. Control Surface and System Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.415 | Ground gust conditions. Control Surface and System Loads | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.421 | Balancing loads. Horizontal Stabilizing and Balancing Surfaces | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.423 | Maneuvering loads. Horizontal Stabilizing and Balancing Surfaces | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.425 | Gust loads. Horizontal Stabilizing and Balancing Surfaces | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.427 | Unsymmetrical loads. Horizontal Stabilizing and Balancing Surfaces | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.441 | Maneuvering loads. Vertical Surfaces | 23-34 | 23-28 | 2 | ✓ Text available |
| §23.443 | Gust loads. Vertical Surfaces | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.445 | Outboard fins [or winglets.] Vertical Surfaces | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.455 | Ailerons. Ailerons; Wing Flaps; and Special Devices | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.457 | Wing flaps. Ailerons; Wing Flaps; and Special Devices | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.459 | Special devices. Ailerons and Special Devices | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.471 | General. Ground Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.473 | Ground load conditions and assumptions. Ground Loads | 23-34 | 23-28 | 2 | ✓ Text available |
| §23.477 | Landing gear arrangement. Ground Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.479 | Level landing conditions. Ground Loads | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.481 | Tail down landing conditions. Ground Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.483 | One-wheel landing conditions. Ground Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.485 | Side load conditions. Ground Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.493 | Braked roll conditions. Ground Loads | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.497 | Supplementary conditions for tail wheels. Ground Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.499 | Supplementary conditions for nose wheels. Ground Loads | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.505 | Supplementary conditions for skiplanes. Ground Loads | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.507 | Jacking loads. Ground Loads | 23-34 | 23-14 | 0 | ✓ Text available |
| §23.509 | Towing loads. Ground Loads | 23-34 | 23-14 | 0 | ✓ Text available |
| §23.511 | Ground load; unsymmetrical loads on multiple-wheel units. Ground Loads | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.521 | Water load conditions. Water Loads | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.561 | General. Emergency Landing Conditions | 23-34 | 23-7 | 4 | ✓ Text available |
| §23.571 | Metallic pressurized cabin structures. Fatigue Evaluation | 23-34 | 23-14 | 3 | ✓ Text available |
| §23.572 | [Metallic] wing, empennage, and associated structures. Fatigue Evaluation | 23-34 | 23-34 | 3 | ✓ Text available |
Design and Construction 14 CFR 23 70 sections
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.601 | General. | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.603 | Materials and workmanship. | 23-34 | 23-23 | 0 | ✓ Text available |
| §23.605 | Fabrication methods. | 23-34 | 23-23 | 0 | ✓ Text available |
| §23.607 | Fasteners. | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.609 | Protection of structure. | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.611 | Accessibility [provisions.] | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.613 | Material strength properties and design values. | 23-34 | 23-23 | 1 | ✓ Text available |
| §23.615 | Design properties. | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.617 | Interchangeability of seamwelded and seamless steel tubing. | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.619 | Special factors. | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.621 | Casting factors. | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.623 | Bearing factors. | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.625 | Fitting factors. | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.627 | Fatigue strength. | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.629 | Flutter. | 23-34 | 23-31 | 3 | ✓ Text available |
| §23.641 | Proof of strength. Wings | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.643 | Rib tests. Wings | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.651 | Proof of strength. Control Surfaces | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.655 | Installation. Control Surfaces | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.657 | Hinges. Control Surfaces | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.659 | Mass balance. Control Surfaces | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.671 | General. Control Systems | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.673 | Primary flight controls. Control Systems | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.675 | Stops. Control Systems | 23-34 | 23-17 | 0 | ✓ Text available |
| §23.677 | Trim systems. Control Systems | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.679 | Control system locks. Control Systems | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.681 | Limit load static tests. Control Systems | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.683 | Operation tests. Control Systems | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.685 | Control system details. Control Systems | 23-34 | 23-17 | 0 | ✓ Text available |
| §23.687 | Spring devices. Control Systems | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.689 | Cable systems. Control Systems | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.693 | Joints. Control Systems | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.697 | Wing flap controls. Control Systems | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.699 | Wing flap position indicator. Control Systems | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.701 | Flap interconnection. Control Systems | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.721 | General. Landing Gear | 23-34 | 23-34 | 0 | ✓ Text available |
| §23.723 | Shock absorption tests. Landing Gear | 23-34 | 23-23 | 1 | ✓ Text available |
| §23.725 | Limit drop tests. Landing Gear | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.726 | Ground load dynamic tests. Landing Gear | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.727 | Reserve energy absorption drop tests. Landing Gear | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.729 | Landing gear extension and retraction system. Landing Gear | 23-34 | 23-26 | 2 | ✓ Text available |
| §23.731 | Wheels. Landing Gear | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.733 | Tires. Landing Gear | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.735 | Brakes. Landing Gear | 23-34 | 23-24 | 3 | ✓ Text available |
| §23.737 | Skis. Landing Gear | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.751 | Main float buoyancy. Floats and Hulls | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.755 | Hulls. Floats and Hulls | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.757 | Auxiliary floats. Floats and Hulls | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.771 | Pilot compartment. Personnel and Cargo Accommodations | 23-34 | 23-14 | 0 | ✓ Text available |
| §23.773 | Pilot compartment view. Personnel and Cargo Accommodations | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.775 | Windshields and windows. Personnel and Cargo Accommodations | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.777 | Cockpit controls. Personnel and Cargo Accommodations | 23-34 | 23-33 | 2 | ✓ Text available |
| §23.779 | Motion and effect of cockpit controls. Personnel and Cargo Accommodations | 23-34 | 23-33 | 1 | ✓ Text available |
| §23.781 | Cockpit control knob shape. Personnel and Cargo Accommodations | 23-34 | 23-33 | 0 | ✓ Text available |
| §23.783 | Doors. Personnel and Cargo Accommodations | 23-36 | 23-36 | 2 | ✓ Text available |
| §23.785 | Seats, berths, litters, safety belts, and shoulder harnesses. Personnel and Cargo Accommodations | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.787 | Baggage and cargo compartments. Personnel and Cargo Accommodations | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.803 | Emergency evacuation. Personnel and Cargo Accommodations | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.807 | Emergency exits. Personnel and Cargo Accommodations | 23-36 | 23-36 | 3 | ✓ Text available |
| §23.811 | Emergency exit marking. Personnel and Cargo Accommodations | 23-36 | 23-36 | 1 | ✓ Text available |
| §23.815 | Width of aisle. Personnel and Cargo Accommodations | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.831 | Ventilation. Personnel and Cargo Accommodations | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.841 | Pressurized cabins. Pressurization | 23-34 | 23-17 | 2 | ✓ Text available |
| §23.843 | Pressurization tests. Pressurization | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.851 | Fire extinguishers. Fire Protection | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.853 | Passenger and crew compartment interiors. Fire Protection | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.859 | Combustion heater fire protection. Fire Protection | 23-34 | 23-27 | 0 | ✓ Text available |
| §23.863 | Flammable fluid fire protection. Fire Protection | 23-34 | 23-23 | 0 | ✓ Text available |
| §23.865 | Fire protection of flight controls, engine mounts, and other flight structure. Fire Protection | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.867 | Lightning protection of structure. Electrical Bonding and Lightning Protection | 23-34 | 23-7 | 0 | ✓ Text available |
Powerplant 14 CFR 23 80 sections
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.901 | Installation. General | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.903 | Engines. General | 23-34 | 23-34 | 0 | ✓ Text available |
| §23.905 | Propellers. General | 23-34 | 23-29 | 2 | ✓ Text available |
| §23.907 | Propeller vibration and fatigue. General | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.909 | Turbocharger systems. General | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.925 | Propeller clearance. General | 23-34 | 23-0 | 3 | ✓ Text available |
| §23.929 | Engine installation ice protection. General | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.933 | Reversing systems. General | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.937 | Turbopropeller-drag limiting systems. General | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.939 | Powerplant operating characteristics. General | 23-34 | 23-18 | 1 | ✓ Text available |
| §23.943 | Negative acceleration. General | 23-34 | 23-18 | 1 | ✓ Text available |
| §23.951 | General. Fuel System | 23-34 | 23-15 | 2 | ✓ Text available |
| §23.953 | Fuel system independence. Fuel System | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.954 | Fuel system lightning protection. Fuel System | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.955 | Fuel flow. Fuel System | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.957 | Flow between interconnected tanks. Fuel System | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.959 | Unusable fuel supply. Fuel System | 23-34 | 23-18 | 1 | ✓ Text available |
| §23.961 | Fuel system hot weather operation. Fuel System | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.963 | Fuel tanks: general. Fuel System | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.965 | Fuel tank tests. Fuel System | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.967 | Fuel tank installation. Fuel System | 23-34 | 23-26 | 2 | ✓ Text available |
| §23.969 | Fuel tank expansion space. Fuel System | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.971 | Fuel tank sump. Fuel System | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.973 | Fuel tank filler connection. Fuel System | 23-34 | 23-18 | 2 | ✓ Text available |
| §23.975 | Fuel tank vents and carburetor vapor vents. Fuel System | 23-34 | 23-29 | 2 | ✓ Text available |
| §23.977 | Fuel tank outlet. Fuel System | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.979 | Pressure fueling systems. Fuel System | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.991 | Fuel pumps. Fuel System Components | 23-34 | 23-26 | 1 | ✓ Text available |
| §23.993 | Fuel system lines and fittings. Fuel System Components | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.994 | Fuel system components. Fuel System Components | 23-34 | 23-29 | 0 | ✓ Text available |
| §23.995 | Fuel valves and controls. Fuel System Components | 23-34 | 23-29 | 0 | ✓ Text available |
| §23.997 | Fuel strainer or filter. Fuel System Components | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.999 | Fuel system drains. Fuel System Components | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.1001 | Fuel jettisoning system. Fuel System Components | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.1011 | General. Oil System | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1013 | Oil tanks. Oil System | 23-34 | 23-15 | 2 | ✓ Text available |
| §23.1015 | Oil tank tests. Oil System | 23-34 | 23-15 | 0 | ✓ Text available |
| §23.1017 | Oil lines and fittings. Oil System | 23-34 | 23-14 | 0 | ✓ Text available |
| §23.1019 | Oil strainer or filter. Oil System | 23-34 | 23-29 | 1 | ✓ Text available |
| §23.1021 | Oil system drains. Oil System | 23-34 | 23-29 | 1 | ✓ Text available |
| §23.1023 | Oil radiators. Oil System | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1027 | Propeller feathering system. Oil System | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.1041 | General. Cooling | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.1043 | Cooling tests. Cooling | 23-34 | 23-21 | 1 | ✓ Text available |
| §23.1045 | Cooling test procedures for turbine engine powered airplanes. Cooling | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.1047 | Cooling test procedures for reciprocating engine powered airplanes. Cooling | 23-34 | 23-21 | 3 | ✓ Text available |
| §23.1061 | Installation. Liquid Cooling | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1063 | Coolant tank tests. Liquid Cooling | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1091 | Air induction system. Induction System | 23-34 | 23-7 | 2 | ✓ Text available |
| §23.1093 | Induction system icing protection. Induction System | 23-34 | 23-29 | 2 | ✓ Text available |
| §23.1095 | Carburetor deicing fluid flow rate. Induction System | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1097 | Carburetor deicing fluid system capacity. Induction System | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1099 | Carburetor deicing fluid system detail design. Induction System | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1101 | [Induction] air preheater design. Induction System | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1103 | Induction system ducts. Induction System | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.1105 | Induction system screens. Induction System | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1111 | Turbine engine bleed air system. Induction System | 23-34 | 23-17 | 0 | ✓ Text available |
| §23.1121 | General. Exhaust System | 23-34 | 23-18 | 2 | ✓ Text available |
| §23.1123 | Exhaust [system.] Exhaust System | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1125 | Exhaust heat exchangers. Exhaust System | 23-34 | 23-17 | 0 | ✓ Text available |
| §23.1141 | Powerplant controls: general. Powerplant Controls and Accessories | 23-34 | 23-18 | 1 | ✓ Text available |
| §23.1143 | Engine controls. Powerplant Controls and Accessories | 23-34 | 23-29 | 2 | ✓ Text available |
| §23.1145 | Ignition switches. Powerplant Controls and Accessories | 23-34 | 23-18 | 1 | ✓ Text available |
| §23.1147 | Mixture controls. Powerplant Controls and Accessories | 23-34 | 23-33 | 1 | ✓ Text available |
| §23.1149 | Propeller speed and pitch controls. Powerplant Controls and Accessories | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1153 | Propeller feathering controls. Powerplant Controls and Accessories | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1155 | Turbine engine reverse thrust and propeller pitch settings below the flight
regime. Powerplant Controls and Accessories | 23-34 | 23-7 | 0 | ✓ Text available |
| §23.1163 | Powerplant accessories. Powerplant Controls and Accessories | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.1165 | Engine ignition systems. Powerplant Controls and Accessories | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.1182 | Nacelle areas behind firewalls. Powerplant Fire Protection | 23-34 | 23-14 | 0 | ✓ Text available |
| §23.1183 | Lines, fittings and components. Powerplant Fire Protection | 23-34 | 23-29 | 1 | ✓ Text available |
| §23.1189 | Shutoff means. Powerplant Fire Protection | 23-34 | 23-29 | 1 | ✓ Text available |
| §23.1191 | Firewalls. Powerplant Fire Protection | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.1192 | Engine accessory compartment diaphragm. Powerplant Fire Protection | 23-34 | 23-14 | 0 | ✓ Text available |
| §23.1193 | Cowling and nacelle. Powerplant Fire Protection | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.1195 | Fire extinguishing systems. Powerplant Fire Protection | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.1197 | Fire extinguishing agents. Powerplant Fire Protection | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.1199 | Extinguishing agent containers. Powerplant Fire Protection | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.1201 | Fire extinguishing system materials. Powerplant Fire Protection | 23-34 | 23-34 | 1 | ✓ Text available |
| §23.1203 | Fire detector system. Powerplant Fire Protection | 23-34 | 23-34 | 2 | ✓ Text available |
Equipment 14 CFR 23 46 sections
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.1301 | Function and installation. General | 23-34 | 23-20 | 1 | ✓ Text available |
| §23.1303 | Flight and navigation instruments. General | 23-34 | 23-17 | 3 | ✓ Text available |
| §23.1305 | Powerplant instruments. General | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.1307 | Miscellaneous equipment. General | 23-34 | 23-23 | 2 | ✓ Text available |
| §23.1309 | Equipment, systems, and installations. General | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.1321 | Arrangement and visibility. Instruments: Installation | 23-34 | 23-20 | 2 | ✓ Text available |
| §23.1322 | Warning, caution, and advisory lights. Instruments: Installation | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.1323 | Airspeed indicating system. Instruments: Installation | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.1325 | Static pressure system. Instruments: Installation | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.1327 | Magnetic direction indicator. Instruments: Installation | 23-34 | 23-20 | 0 | ✓ Text available |
| §23.1329 | Automatic pilot system. Instruments: Installation | 23-34 | 23-23 | 2 | ✓ Text available |
| §23.1331 | Instruments using a power source. Instruments: Installation | 23-34 | 23-0 | 2 | ✓ Text available |
| §23.1335 | Flight director [systems.] Instruments: Installation | 23-34 | 23-20 | 0 | ✓ Text available |
| §23.1337 | Powerplant instruments installation. Instruments: Installation | 23-34 | 23-18 | 3 | ✓ Text available |
| §23.1351 | General. Electrical Systems and Equipment | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.1353 | Storage battery design and installation. Electrical Systems and Equipment | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.1357 | Circuit protective devices. Electrical Systems and Equipment | 23-34 | 23-20 | 1 | ✓ Text available |
| §23.1361 | Master switch arrangement. Electrical Systems and Equipment | 23-34 | 23-20 | 2 | ✓ Text available |
| §23.1365 | Electric cables and equipment. Electrical Systems and Equipment | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.1367 | Switches. Electrical Systems and Equipment | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1381 | Instrument lights. Lights | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1383 | Taxi and landing lights. Lights | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1385 | Position light system installation. Lights | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.1387 | Position light system dihedral angles. Lights | 23-34 | 23-12 | 1 | ✓ Text available |
| §23.1389 | Position light distribution and intensities. Lights | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1391 | Minimum intensities in the horizontal plane of [position lights.] Lights | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1393 | Minimum intensities in any vertical plane [of position lights.] Lights | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1395 | Maximum intensities in overlapping beams of [position lights.] Lights | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1397 | Color specifications. Lights | 23-34 | 23-11 | 0 | ✓ Text available |
| §23.1399 | Riding light. Lights | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1401 | Anticollision light system. Lights | 23-34 | 23-20 | 1 | ✓ Text available |
| §23.1411 | General. Safety Equipment | 23-34 | 23-17 | 1 | ✓ Text available |
| §23.1413 | Safety belts and harnesses. Safety Equipment | 23-34 | 23-22 | 0 | ✓ Text available |
| §23.1415 | Ditching equipment. Safety Equipment | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1416 | Pneumatic de-icer boot system. Safety Equipment | 23-34 | 23-23 | 0 | ✓ Text available |
| §23.1419 | Ice protection. Safety Equipment | 23-34 | 23-14 | 1 | ✓ Text available |
| §23.1431 | Electronic equipment. Miscellaneous Equipment | 23-34 | 23-0 | 3 | ✓ Text available |
| §23.1435 | Hydraulic systems. Miscellaneous Equipment | 23-34 | 23-14 | 2 | ✓ Text available |
| §23.1437 | Accessories for multiengine airplanes. Miscellaneous Equipment | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1438 | Pressurization and pneumatic systems. Miscellaneous Equipment | 23-34 | 23-20 | 0 | ✓ Text available |
| §23.1441 | Oxygen equipment and supply. Miscellaneous Equipment | 23-34 | 23-9 | 1 | ✓ Text available |
| §23.1443 | Minimum mass flow of supplemental oxygen. Miscellaneous Equipment | 23-34 | 23-9 | 2 | ✓ Text available |
| §23.1447 | Equipment standards for oxygen dispensing units. Miscellaneous Equipment | 23-34 | 23-30 | 3 | ✓ Text available |
| §23.1449 | Means for determining use of oxygen. Miscellaneous Equipment | 23-34 | 23-9 | 0 | ✓ Text available |
| §23.1450 | Chemical oxygen generators. Miscellaneous Equipment | 23-34 | 23-20 | 0 | ✓ Text available |
| §23.1461 | Equipment containing high energy rotors. Miscellaneous Equipment | 23-34 | 23-20 | 1 | ✓ Text available |
Operating Limitations and Information 14 CFR 23 29 sections
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.1501 | General. | 23-34 | 23-21 | 0 | ✓ Text available |
| §23.1505 | Airspeed limitations. | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.1507 | (Operating) maneuvering speed. | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1511 | Flap extended speed. | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1513 | Minimum control speed. | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1519 | Weight and center of gravity. | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1521 | Powerplant limitations. | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.1523 | Minimum flight crew. | 23-34 | 23-34 | 0 | ✓ Text available |
| §23.1525 | Kinds of operation. | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1527 | Maximum operating altitude. | 23-34 | 23-7 | 1 | ✓ Text available |
| §23.1529 | Instructions for Continued Airworthiness. | 23-34 | 23-26 | 0 | ✓ Text available |
| §23.1541 | General. Markings and Placards | 23-34 | 23-21 | 0 | ✓ Text available |
| §23.1543 | Instrument markings: general. Markings and Placards | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1545 | Airspeed indicator. Markings and Placards | 23-34 | 23-23 | 2 | ✓ Text available |
| §23.1547 | Magnetic direction indicator. Markings and Placards | 23-34 | 23-20 | 0 | ✓ Text available |
| §23.1549 | Powerplant [and auxiliary power unit instruments.] Markings and Placards | 23-34 | 23-28 | 1 | ✓ Text available |
| §23.1551 | Oil quantity indicator. Markings and Placards | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1553 | Fuel quantity indicator. Markings and Placards | 23-34 | 23-0 | 1 | ✓ Text available |
| §23.1555 | Control markings. Markings and Placards | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.1557 | Miscellaneous markings and placards. Markings and Placards | 23-34 | 23-23 | 1 | ✓ Text available |
| §23.1559 | Operating limitations placard. Markings and Placards | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.1561 | Safety equipment. Markings and Placards | 23-34 | 23-0 | 0 | ✓ Text available |
| §23.1563 | Airspeed placards. Markings and Placards | 23-34 | 23-7 | 3 | ✓ Text available |
| §23.1567 | Flight maneuver placard. Markings and Placards | 23-34 | 23-21 | 2 | ✓ Text available |
| §23.1581 | General. Airplane Flight Manual and Approved Manual Material | 23-34 | 23-34 | 2 | ✓ Text available |
| §23.1583 | Operating limitations. Airplane Flight Manual and Approved Manual Material | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.1585 | Operating procedures. Airplane Flight Manual and Approved Manual Material | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.1587 | Performance information. Airplane Flight Manual and Approved Manual Material | 23-34 | 23-34 | 3 | ✓ Text available |
| §23.1589 | Loading information. Airplane Flight Manual and Approved Manual Material | 23-34 | 23-0 | 2 | ✓ Text available |
Appendix 14 CFR 23 5 sections ! 2 text missing
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| 14 CFR 23 A23 | Appendix A to Part 23 - Simplified Design Load Criteria | 23-34 | 23-28 | 1 | ✓ Text available |
| 14 CFR 23 C23 | Appendix C to Part 23 - Basic Landing Conditions | 23-34 | 23-7 | 0 | ! Text missing |
| 14 CFR 23 D23 | Appendix D to Part 23 - Wheel Spin-Up and Spring-Back Loads | 23-34 | 23-0 | 1 | ! Text missing |
| 14 CFR 23 F23 | Appendix F to Part 23 - Test Procedure | 23-34 | 23-34 | 2 | ✓ Text available |
| 14 CFR 23 G23 | Appendix G to Part 23 - Instructions for Continued Airworthiness | 23-34 | 23-34 | 1 | ✓ Text available |