JASC 5744

Service difficulty reports · 2,730

Reports filed under 5744 · Wing, Control Surface Attach Fittings, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5744'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201508172590Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.597", FINAL HOLE DIAMETER 0.631", MAX ALLOWABLE HOLE DIAMETER 0.621". OVERSIZED BUSHIAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172589Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.597", FINAL HOLE DIAMETER 0.631", MAX ALLOWABLE HOLE DIAMETER 0.621". OVERSIZED BUSHINGAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172588Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.408", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATEAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172587Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.407", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATEDAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172586Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 10 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.668", FINAL HOLE 0.691", MAXIMUM ALLOWABLE HOLE 0.667". OVERSAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172585Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-09. EXISTING THICKNESS UPPER 0.426", LOWER 0.448", MATERIAL REMOVED UPPER 0.006", LOWER 0.006", REMAINING THICKNESS UPPER 0.420", LOWER 0.442Aug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172584Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.328", MATERIAL REMOVED 0.013", REMAINING THICKNESS 0.315", MINIMUM ALLOWABLE THICKNESS 0.320Aug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172583Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.253", FINAL HOLE 1.257", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED BAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172582Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.258", FINAL HOLE 1.282", MAXIMUM ALLOWABLE HOLE 1.258". OVEAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172581Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.253", FINAL HOLE 1.257, MAXIMUM ALLOWABLE HOLE 1.220". OVERAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172580Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.365", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.361", MAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172579Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.357", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.353", MAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172578Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.522", FINAL HOLE 0.591", MAXIMUM ALLOWABLE HOLE 0.584". SAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172577Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.723", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.717", MIAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508072509Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072508Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072507Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072506Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072505Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072504Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072502Hinge Bracket · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, BARREL NUT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED, FOUND WITHIN LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072501Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =0.5Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072500Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE NR 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072499Hinge · corrodedLEFT WING, WING SIDE, OTBD FLAP OTBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =2.3105", FINAL HOLE DIAMETER =2.334", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIR BUSHING Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072497Hinge Bracket · corrodedLEFT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW CMM 57-44-08. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072496Hinge · corrodedLEFT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE, FOUND CORROSIONS. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.219", FINAL HOLE DIAMETER =1.252", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220".Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072495Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE INBD ACTUATOR HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.215", FINAL HOLE DIAMETER =1.254", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220". REPAIRED BAug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072494Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER =2.309", FINAL HOLE DIAMETER =2.336", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIRED BUSHING, Aug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072493Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.643", FINAL HOLE DIAMETER =0.721", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIREAug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508072492Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.703", FINAL HOLE DIAMETER =0.723", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIREDAug 7, 2015 · N529FE · Doug MD11FSDR FDEA201508052482Mount · corrodedLEFT WING, WING SIDE OTBD FLAP HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =0.591", FINAL HOLE DIAMETER =0.599", MAXIMUM ALLOWABLE HOLE DIAMETER =0.584". AIR BUSHING FAug 5, 2015 · N529FE · Doug MD11FSDR A6WA201542671Mount Bracket · crackedSPOILER MOUNT BRACKET CRACKED.Apr 25, 2015 · N461AW · Cndair CL6002B19SDR DALA2015022401614Bracket · crackedCRACKED INTERNAL BRACKET ON NR 8 SLAT TRACK HOUSING AT LT WING FIXED L/E STA XRS 260 APPROXIMATELY SLAT TRACK NR 8 AT LT WING WAS REMOVED IAW AMM 27-80-07. INTERNAL BRACKET ON HOUSING OF SLAT TRACK NR 8 AT LW WAS REMOVED, IAW AMM 20-30-01. NEW BRACKET WAS TREFeb 23, 2015 · N980DL · Doug MD88SDR SWIA201540831Hinge · chafedLT WING OTBD FLAP HAS 2 CHAFING MARKS ON LOWER L/E AT CENTER HINGE. C-CHECK, REPAIRED, 2 EA, CHAFED AREAS ON LT WING OTBD FLAP LWR L/E AT THE CENTER HINGE IAW STS EA.Feb 21, 2015 · N755SK · Cndair CL6002C10SDR ASAA2015021410667Fitting · crackedLT WING INBD FLAP OTBD FITTING THAT ATTACHES TO THE INBD FLAP OTBD CANOE ROD END IS CRACKED. ACFT GROUNDED. OPENED ACCESS PANEL 553ET AND DISCONNECTED THE NR 3 FLAP FAIRING AFT SUPPORT ROD FROM BROKEN FITTING. REMOVED HILOC FROM OLD FITTING AND REMOVED CRACFeb 14, 2015 · N549AS · Boeing 7378FHSDR FDEA201502080479Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORROSION. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0315338 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 8, 2015 · N523FE · Doug MD11FSDR FDEA201502050449Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0315333 PART 1 STEP 1 AND 1C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 5, 2015 · N523FE · Doug MD11FSDR FDEA201502050448Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, SIDE ATTACH LOWER BORE FOUND CORROSION. REPAIR CARRIED OUT AS PER EA 1-5750-T0315333 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Feb 5, 2015 · N523FE · Doug MD11FSDR FDEA201502050447Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE ATTACH UPPER BORE FOUND CORROSION. RIGHT HAND WING OUTBOARD FLAP OUTBOARD FORWARD HINGE BRACKET SIDE ATTACH UPPER BORE NR 7 REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09 EXISTING HOLE DIA.: 0.3Feb 5, 2015 · N523FE · Doug MD11FSDR FDEA201502050446Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, LOWER OTBD STUD ATTACH BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0315333 PART 1 STEPS 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 5, 2015 · N523FE · Doug MD11FSDR FDEA201502050445Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, LOWER INBD STUD ATTACH BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0315333 PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 5, 2015 · N523FE · Doug MD11FSDR FDEA201502040433Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315335 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 4, 2015 · N523FE · Doug MD11FSDR FDEA201502040429Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315335 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 4, 2015 · N523FE · Doug MD11FSDR FDEA201502040428Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, LOWER OTBD STUD ATTACH BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315335 PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 4, 2015 · N523FE · Doug MD11FSDR FDEA201502040427Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, LOWER INBD STUD ATTACH BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315335 PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 4, 2015 · N523FE · Doug MD11FSDR FDEA201502040426Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE BRACKET PIVOT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315337 PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 4, 2015 · N523FE · Doug MD11FSDR FDEA201502030419Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315337 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11FSDR FDEA201502030418Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REPAIRED IAW EA 1-5750-T0315337 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11FSDR FDEA201502030416Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA1-5750-T0315330 REV A PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11FSDR FDEA201502030415Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0315330 REV A PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F
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