Boeing 727-22

Service difficulty reports · 1,282

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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 aircraft_model_key = '72722'
  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 96FDEA00155Skin · dentedDENT TO SKIN DUE TO TOOL BOX AT STA 1083 AND BETWEEN STR 28 - 29L. REPAIRED DAMAGED SKIN AT BS 1083, BETWEEN STR 28 - 29L PER FEDEX SRM 53-30-3 PER ENGINE REPAIR REQUEST REPLY. MFG PART NUMBER M502776.Jan 31, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00148Shear Tie · corrosionCORROSION (C53-111-01, -3), AFT CARGO ON SHEAR TIE AT BS 1030 RBL 4 WL 138.5. REPAIRED SHEAR TIE AT BS 1030 RBL 4 WL 138.5 AS PER FEDEX SRM 53-10-4.Jan 30, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00147Floor Beam · corrosionCORROSION ON FLOOR BEAM (C 53-224-01, -1), BS 312 WL 208 LBL 46. REMOVED CORROSION ON FLOOR BEAM AT BS 312 WL 208 LBL 46 OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FLOOR BEAM PER FEDEX SRM 53-10-8.Jan 30, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00165Stringer · corrodedCORROSION (C53-111-01-2), ON STR 27L BS 590 WL 152. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR SPLICE AND SHIM AT BS 590 STR 27L WL 152 PER FEDEX SRM 53-10-3.Jan 29, 1996 · N193FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00164Stringer · misdrilledTRAMCO RESPONSIBILITY 9601-59 WHILE WORKING NR0048 SKIN REPAIR MISDRILLED STR AT BS 410 STR 20R. REMOVED DAMAGED STR SECTION BS 410 STR 20R, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-3.Jan 29, 1996 · N193FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00190Floor Beam · corrodedCORROSION (C53-224-06), ON FLOOR BEAM AT BS 600 RBL 10 WL 208. REMOVED CORRODED SECTION FLOOR BEAM, FABRICATED REPAIR ANGLES AND INSTALLED ALL WORK DONE PER FEDEX SRM 53-10-8.Jan 28, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00163Skin · mech damageSKIN HAS TWO DRILL STARTS AT BS 255.5 WL 169 RT SIDE. FABRICATED SKIN DOUBLER PER FEDEX 53-30-1 AT BS 255.5 WL 169 RT SIDE.Jan 28, 1996 · N193FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00137Fitting · corrosionCORROSION ON STR TO FRAME TIE AT BS 360 STR 20L. REMOVED AND REPLACED STR TIE AT BS 360 20L, DUE TO CORROSION OUT OF LIMITS.Jan 26, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00136Fitting · crackedLT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IS CRACKED. REPAIRED LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IAW FEDEX EA 7-5510-26907.Jan 26, 1996 · N169FE · Boeing 72722 · Vertical StabilizerSDR 96FDEA00135Stringer · delaminationDELAMINATION OF SKIN LAP STRINGER 19L BS 360 TO 368. REMOVED FASTENERS IN SKIN LAP AT STR 19L. UPON REMOVAL OF FASTENERS FOUND NO FURTHER INDICATIONS OF DELAMINATION. INSTALLED NEW STR TIE AND INSTALLED STR 19 SPLICE. ALL WORK DONE IAW FEDEX SRM 53-10-3.Jan 26, 1996 · N169FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00120Transmitter · wornAFTER TAKEOFF DURING FLAP RETRACTION. THE OUTBOARD FLAPS BECAME ASYMMETRICAL BETWEEN THE ZERO AND 2 DEGREE INDICATOR, REPEAT WRITE UP. FOUND RT OUTBOARD TRANSMITTER SECURING COLLAR LOOSE, ADJUSTED TRANSMITTER AND TIGHTENED COLLAR PER MM 27-52-12. RAN FLAPS Jan 24, 1996 · N191FE · Boeing 72722 · Trailing Edge Flap Control SystemSDR 96FDEA00077Fitting · crackedDURING UT INSP, CRACK IND FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913.Jan 19, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00076Fitting · crackedCRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER EWO NR 96-2043.Jan 19, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00075Skin · lightning strikeLIGHTNING STRIKES AT BS 706, 793, 824 AND 888 BETWEEN STR 4 AND 5. REPAIRED LIGHTNING STRIKES AT BS 750, 793, 824 BY INSTALLING NEW FASTENERS. REPAIRED BS 888 BY CUTTING OUT DAMAGED AREA AND FABRICATING REPAIR PARTS. INSTALLED IAW 53-30-3.Jan 19, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00074Skin · chafingRT WING I/B FOREFLAP IS CHAFING APPROX 24 INCHES O/B FROM I/B LEADING EDGE. REPAIRED DAMAGE AREA ON RT WING I/B FOREFLAP APPROX 24 INCHES O/B FROM I/B LEADING EDGE.Jan 19, 1996 · N169FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00078Skin · corrodedCORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW STR 9R PER FEDEX EA 7-5310-26957.Jan 18, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00067Te Skin · disbondedRIGHT WING INBD FORE FLAP UPPER SURFACE HAS DISBOND ON T/E AREA MARKED. REPAIRED RT WING INBOARD FORE FLAP IAW SRM 51-40-6.Jan 18, 1996 · N169FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00066Stringer · corrodedCORROSION (C53-224-03-1/2) ON STR 22R, BS 396. REMOVED CORROSION AT BS 396, STR 22R. REMOVED IN A 1 INCH BY 2 INCH AREA. ORIGINAL METAL THICKNESS IS .040 INCH. REMOVED .009 INCH, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED AND INSTALLED REJan 18, 1996 · N169FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00065Stiffener · corrodedCORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.Jan 17, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00060Skin · gougedTHERE'S A GOUGE ON THE RT WING FOREFLAP UPPER SURFACE ABOVE THE NR 8 FLAP TRACK. REMOVED AND REPLACED DAMAGE ON O/B RT WING FOREFLAP IAW FEDEX SRM 51-40-6.Jan 17, 1996 · N169FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00064Stiffener · corrodedCORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER, BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.Jan 15, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96ZZZX2492Frame · corrodedFUSELAGE FRAME AT BS 540 AT STR 27L HAS EXFOLIATION CORROSION ON VERTICAL PORTION OF FRAME. CORROSION HAS LEFT A 1.50 INCH HOLE IN FRAME.Jan 8, 1996 · N40482 · Boeing 72722 · Fuselage Main, FrameSDR 96ZZZX2491Skin · corrodedDURING ROUTINE INSPECTION OF AIRCRAFT, 3 EACH FASTENER HEADS FOUND WITH HEADS POPPED OFF ALONG THE SKIN LAP JOINT AT STR 28R BETWEEN BS 420 - BS 460. ALSO, BULGING OF THE SKIN WAS EVIDENT AROUND THE FASTENERS INDICATING CORROSION. AREA WAS REPAIRED PER BOEINJan 8, 1996 · N40482 · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96ZZZX2490Skin · corrodedDURING INSPECTION OF AIRCRAFT, A FASTENER WITH ITS HEAD POPPED OFF AND 2 EACH FASTENERS AFT OF THE FIRST FASTENER WERE ALMOST PULLED THROUGH THE FUSELAGE SKIN AT BS 480 NEAR STR 29L. INTERNAL INSPECTION REVEALED CORROSION OF THE FUSELAGE SKIN AROUND THE FASTEJan 8, 1996 · N40482 · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96ZZZX2489Stringer · corrodedDURING ROUTINE INSPECTION OF AIRCRAFT, 5 EACH FASTENER HEADS WERE FOUND PULLING THROUGH THE SKIN ALONG FUSELAGE STR 28R AND BS 1030, BS 1060, AND FUSELAGE SKIN WAS FOUND BULGING DUE TO CORROSION. ONCE THE AREA WAS DISASSEMBLED, DAMAGE WAS FOUND TO EXTEND BACKJan 8, 1996 · N40482 · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96ZZZX2488Seat Track · corrodedDURING ROUTINE INSPECTION OF AIRCRAFT, THE FORWARD CARGO COMPARTMENT'S LEFT TIE-DOWN TRACK WAS FOUND CORRODED OVER A 20 INCH AREA CENTERED AROUND BS 540. EVALUATION OF PART COST VERSUS REPAIR COST LED TO REPLACEMENT OF PART WITH NEW.Jan 8, 1996 · N40482 · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00017Dn Lock Switch · failedNOSE GEAR DID NOT SHOW DOWN AND LOCKED. CYCLED IAW CHECKLIST, SUCCESSFUL 3 DOWN. GEAR HORN SOUNDED CONTINUOUSLY WHEN FLAPS EXTENDED TO 30 DEGREES CONFIRMING GEAR UNSAFE CONDITION. REPLACED NOSE LANDING GEAR LOCK SWITCH IAW MM 32-61-21 AND OPS CHECK GOOD.Jan 5, 1996 · N148FE · Boeing 72722 · Landing Gear Position and WarningSDR 96ZZZX2487T-Chord · corrodedT-CHORD COMMON TO NOSE LANDING GEAR WHEELWELL IN LEFT SIDE OF NOSE COMPARTMENT AT FLOOR LEVEL (WL 170 APPROXIMATELY) WAS FOUND CORRODED IN 6 DIFFERENT AREAS. ALSO, NOSE GEAR WALL ABOVE T-CHORD WAS FOUND TO HAVE SURFACE CORROSION. CORROSION RANGED FROM SURFACJan 3, 1996 · N40482 · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01811Floorbeam · corrosionCORROSION (C53-224-02), AROUND NUTPLATE HOLES AT BS 312 LBL 2 TO 18 WL 208.1. REPAIRED CORRODED AREA AT BS 312 LBL 2 TO 18 WL 208.1 IAW FEDEX SRM 53-10-8.Nov 27, 1995 · N191FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01810Threshold · corrodedCORROSION UNDER NUTPLATES ON THRESHOLD STRAP, STA 524 TO 576 RBL 24 WL 156, FWD BAY. REPLACED STRAP FROM BS 520 TO 600 RBL 24 WL 156.Nov 27, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01815Frame · damagedDURING INSPECTION PER EO 7-5310-7-3367, A FREEZE PLUG WAS FOUND PREVIOUSLY INSTALLED IN A FASTENER HOLE AT WL 208.10, IN THE LT 825.95 FRAME WEB FLANGE AND REINFORCING CHORD. OLD FREEZE PLUG WAS FOUND DAMAGED. REMOVED OLD FREEZE PLUG, OVERSIZED HOLE AND INSTNov 23, 1995 · N191FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01814Stringer · corrodedFOUND CORROSION IN CHANNEL OF STR 28R RBL 14.5 WL 155 BS 1105. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 53-10-03 FIG 1.Nov 23, 1995 · N191FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA01813Sill Web · buckledFOUND DOOR SILL WEB BUCKLED AT BS 1070 RBL 22 WL 152.5. UPON FURTHER INVESTIGATION OF DAMAGE DETERMINED THAT THIS REPAIR IS NOT ODR REPORTABLE PER FEDEX GMM SECTION.Nov 23, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01812Forging · crackedFOUND CRACKS ON STA 740 FORGING LT. THREE LOCATIONS BETWEEN STR 23 TO 24L, BETWEEN STR 18 TO 19L AND BETWEEN STR 19 TO 20L. REPAIRED DAMAGED AREAS PER FEDEX EA 7-5310-26123.Nov 23, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01787Web · crackedFOUND CRACK ON STA 740 WEB AT RBL 42, WL 185 (CENTER TANK). REPAIRED CRACK ON STA 740 WEB AT RBL 42, WL 185 (CENTER TANK) IAW EA 7-5710-26212.Nov 21, 1995 · N191FE · Boeing 72722 · Wing Miscellaneous StructureSDR 95FDEA01744Web · corrodedWHILE REMOVING BS 870 LOWER WING CHORD, FOUND BS 870 WEB TO BE SEVERELY CORRODED.Nov 14, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01745Stringer · chippedWHILE INSTALLING FASTENERS IN BELLY SKIN DISCOVERED CHIPPED OUT AREA ON STR 27R AT BS 1140 RBL 21 WL 153.Nov 13, 1995 · N191FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA01742Channel · corrodedCORROSION (C53-111-01, 3) ON SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5. REMOVED AND REPLACED SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5, DUE TO CORROSION BEING OUT OF LIMITS PER FEDEX SRM 53-10-01.Nov 13, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01741Floorbeam · corrodedCORROSION (C53-111-01-3), ON LOWER FLANGE OF FLOORBEAM BS 1110 RBL 28 TO LBL 31 WL 200. REMOVED AND REPLACED ENTIRE LWR CHORD OF THE BS 1110 FLOORBEAM PER FEDEX EA 7-5310-20796.Nov 13, 1995 · N191FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01739Stringer · crackedIN THE AFT GALLEY AT BS 1050 LBL 60 WL 176, THERE IS A CRACK IN THE LOWER FLANGE OF STR 21 UNDER THE FAIL-SAFE CHORD. REPAIRED CRACKED STR AT BS 1050 LBL 60 WL 176 ON LOWER FLANGE OF STR 21L PER FEDEX SRM 53-10-3 FIG 1 AND FAIL-SAFE CHORD PER FEDEX SRM 51-40-Nov 13, 1995 · N191FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA01738Floorbeam · corrosionCORROSION ON FLOORBEAM LOWER CHORD BS 540 WL 200 LBL 22 TO RBL 22 WILL REQUIRE REMOVAL OF DOOR LATCH WEB. MECH REMOVED CORROSION FROM LOWER CHORD OF FLOORBEAM BS 540 RBL 22 TO LBL 22 WL 200 MATERIAL LOSS IS BEYOND LIMITS IAW FEDEX SRM 53-10-1 AT RBL 9 AND RBLNov 13, 1995 · N191FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01737Shear Tie · crackedWHILE WORKING NR 0349, FOUND SHEAR TIE AT BS 1130 RBL 2 WL 148.5 TO BE CRACKED AND CORRODED. REMOVED CRACKED AND CORRODED SHEAR TIE FLANGE ANGLE AT BS 1130 RBL 2 WL 148.5, FABRICATED AND INSTALLED TWO REPAIR ANGLES AND ONE SUPPORT CLIP. ALL WORK ACCOMPLISHEDNov 13, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01736Fuel Cell Skin · corrosionWHILE WORKING NR O494, FOUND CORROSION ON TOP SIDE OF LOWER FUEL CELL SKIN RBL 41 WL 162.5 BS 870. REMOVED CORROSION FROM TOP SIDE OF LOWER FUEL CELL SKIN RBL 41 WL 162.5 BS 870. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-30-1 AND REPAIRED PER EA 7-5730-2615Nov 13, 1995 · N191FE · Boeing 72722 · Fuel StorageSDR 95FDEA01743Stringer · chippedWHILE INSTALLING FASTENERS IN BELLY SKIN DISCOVERED CHIPPED OUT AREA ON STR 27R BS 1140 RBL 21 WL 153. REPAIRED DAMAGED AREA ON STR 27R AT BS 1140 RBL 21 WL 153 PER FEDEX EA 7-5310-28199.Nov 11, 1995 · N191FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA01740Lwr Chord · corrosionCORROSION (C53-111-01-3), IN THE AFT BAY AT BS 1030 WL 200 FROM LBL 20 TO RBL 14, THERE IS CORROSION IN THE NUTPLATE HOLES. REMOVED CORROSION, FABRICATED NEW REPAIR ANGLE AND INSTALLED FASTENERS. ALL WORK DONE IAW FEDEX EA 7-5310-26152.Nov 11, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01704Frame · damagedFOUND 2 DAMAGED FASTENER HOLES ON FRAME, STA 580 STR 22 TO 24 AND 25L, FWD BAY. REPAIRED BY CUTTING OUT DAMAGED AREAS ON 550 BS FRAME ABOVE STR 22, 24, AND 25L, FABRICATED, ALODINED, PRIMED AND INSTALLED THREE REPAIR DOUBLERS PER FEDEX SRM 51-40-3 AND 53-10-2Nov 8, 1995 · N191FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01703Doorway Frame · misdrilledDOUBLE HOLE IN FRAME STA 1110, AFT SIDE OF DOORWAY UNDER WEB STR 27R. REPAIRED DOUBLE HOLE IN FRAME AT STA 1110, AFT SIDE OF CARGO DOORWAY UNDER WEB STR 27R AS PER FEDEX SRM 51-40-3 FIG 1.Nov 8, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01702Doorway Frame · misdrilledDOUBLE HOLE IN FRAME STA 1056 FWD SIDE OF CARGO DOORWAY UNDER WEB STR 27R. REPAIRED DOUBLE HOLE IN FRAME AT STA 1056 FWD SIDE OF CARGO DOORWAY UNDER WEB STR 27R AS PER FEDEX SRM 51-40-3 AND 53-10-4.Nov 8, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01701Channel · corrodedCORROSION (C53-1111-01, 3), ON SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5. REMOVED AND REPLACED SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5, DUE TO CORROSION BEING OUT OF LIMITS PER FEDEX SRM 53-10-01.Nov 8, 1995 · N191FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01689Frame · double holeDOUBLE HOLE IN FRAME BS 520 STR 25L. REPAIRED DOUBLE HOLE IN FRAME AT BS 520 STR 25L PER FEDEX SRM 51-40-3.Nov 6, 1995 · N191FE · Boeing 72722 · Fuselage Main, Frame
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