Boeing 727-25

Service difficulty reports · 827

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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 = '72725'
  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 95FDEA00477Floorbeam · corrosionCORROSION IN THE FWD CARGO BAY THERE IS CORROSION ON LOWER FLANAGE OF FLOORBEAM AT NUTPLATE LOCATION BS 660 RBL 14 WL 200. BLENDED AND REMOVED CORROSION ON FLOORBEAM, ORIGINAL THICKNESS OF MATERIAL 133 REMOVED .027 5 BY 1 AREA, FLOORBEAM, OUT OF LIMITS PER FEApr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00476Skin · crackedCORROSION AND GOUGE ON SKIN BS 1183 TO 1342 STR 20 TO 27L. REMOVED CORROSION FROM SKIN AND INSTALLED DOUBLER OVER AREA WHERE SKIN WAS REMOVED DUE TO GOUGE. IAW FEDEX SRM 53-30-3.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA00475Web · corrodedCORROSION UNDER WEB 254 TO 259 RBL 48 WL 224. REMOVED CORRODED DOUBLER STA 254 TO 259 RBL 48 WL 224, FABRICATED NEW DOULBER, ALODINED, PRIMED, INSTALLED.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00474Seat Track · corrodedCORROSIN ON SEAT TRACK BS 48 RBL 45 WL 208. ALSO, AT BS 578 RBL 45 SHEARED FASTENER AT 480 RBL 45. REMOVED AND REPLACED SEAT TRACK AT RBL 45, WL 208 BS 480 TO 580 IAW FEDEX SRM 53-10-5. ALSO, REPLACED SHEARED FASTENER AT RBL 45, BS 480 REINSTALL AND REMOVEDApr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00473Stiffener · corrodedBS 254 WL 173, RBL 25 HORIZONTAL STIFFENER IS CORRODED. BLENDED OUT AND REMOVED CORROSION, CUT AND TRIMMED OFF FLANGE. FABRICATED A NEW REPAIR PART, ALODINED, PRIMED, PAINTED PART, INSTALLED PART WET WITH SEALANT. ALL WORK ACCOMPLISHED IAW FEDEX (EA 7-5310-Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00472Hinge · crackedRT WING O/B AILERON, OTBD CENTER HINGE FITTING CRACKED. REMOVED CRACKED FITTING, INSTALLED NEW FITTING.Apr 25, 1995 · N155FE · Boeing 72725 · AileronsSDR 95FDEA00471Skin · crackedBS 251.6 STR 22R, POSSIBLE CRACK IN SKIN AT FASTENER. REPAIRED CRACK IN SKIN PER FEDEX SRM 53-30-3 BS 251.6 STR 22R.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA00470Frame · crackedCRACKED FRAME AT BS 1090 LBL 22 UNDER FLOOR TO SIDEWALL SUPPORT WL 150. REPAIRED CRACKED FRAME PER FEDEX SRM 51-40-3.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00469Blkhd Web · carckedCRACK IN 950 BULKHEAD RBL 22 WL 183. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 183 PER FEDEX SRM 53-10-9.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, BulkheadSDR 95FDEA00468Blkhd Web · crackedCRACK IN 950 BULKHEAD RBL 22 WL 166. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 166 PER FEDEX SRM 53-10-9.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, BulkheadSDR 95FDEA00467Skin · dentedBS 460-520 BETWEEN STR 20R TO 21R THERE IS A DENT IN SKIN THAT OIL CANS. CUT OUT DAMAGED AREA FABRICATED REPAIR DOUBLER ALODINE AND PRIMERED, INSTALLED WET WITH SEALANT, INSTALLED FASTENERS IAW FEDEX SRM 53-30-3.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA00466Floorbeam · corrodedCORROSION (72C235-02) ON FLOORBEAM AT BS 680 RBL 10 WL 208. REMOVED AND REPLACED TOP CHORD ON FLOORBEAM AT BS 680 LBL 10 TO RB 15, WL 208 PER FEDEX SRM 53-10-8.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00465Skin · lightning strikeBS 294.5 BETWEEN STR 24L AND 25L, THERE IS A LIGHTNING STRIKE. BLENDED AREA BS 294.5 BETWEEN STR 24L TO 25L AND FABRICATED DOUBLER, INSTALLED PER FEDEX SRM 53-30-3.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA00464Failsafe Chord · crackedCRACKED FAILSAFE CHORD BS 1110 STR 24L. REPAIRED CRACKED FAILSAFE CHORD AT BS 1110 STR 24L AS PER FEDEX SRM 51-40-4.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00463Bulkhead · crackedCRACK IN 950 BULKHEAD LBL 41, WL 182. REPAIRED CRACK IN 950 BULKHEAD AT LBL 41 WL 182 IAW FEDEX 727 SRM 53-10-9.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, BulkheadSDR 95FDEA00462Frame · damagedDAMAGED FRAME AT WL 300, STA 1110, STR 2L PLUS 2 INCHES. REMOVED DAMAGED AREA FROM FRAME AT WL 300 STA 1110 STR 2L, FABRICATED AND INSTALLED DOUBLER PER FEDEX SRM 53-10-4 PG 2.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00461Shear Tie · crackedCORROSION ON SHEAR TIE BS 1148, LBL 22, WL 153. REMOVE AND REPLACED SHEAR TIE AT BS 1148, LBL 22, WL 153 AS PER FEDEX SRM 53-10-4.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00460Stringer · crackedCRACKED STR 22L, BS 1030. CUT OUT DAMAGED AREA FABRICATED REPAIR PARTS, INSTALLED REPAIR PARTS NET WITH SEAL AND INSTALLED FASTENERS, ALL WORK DONE IN ACCORDANCE WITH FEDEX SRM 53-10-3 AT BS 1030 STR 22L. MFG P/N M377459, BAC1498132, M424422.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 95FDEA00459Bulkhead · cracked2 CRACKS IN 950 BULKHEAD LBL 5 AND RBL 5 WL 174. REPAIRED CRACKS IN 950 BLUKHEAD AT LBL 5 AND RBL 5 WL 174 PER FEDEX SRM 53-10-9 FIG 2.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, BulkheadSDR 95FDEA00458Fitting · separatedSUSPECT INDICATIONS FOUND AT BS 870 RT TERMINAL FITTING DURING UT INSP. REQUIRE REMOVAL OF FWD AND AFT SPLICE PLATES TO VERIFY INDICATIONS WITH HFEC. REPAIRED WEB SEPARATION IN BS 870 RT TERMINAL FITTING IAW FEDEX EA 7-5310-24491.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00457Stringer · corrodedCORROSION ON STR 22L, BS 1165. REPAIRED STR 22L AT BS 1165 PER FEDEX SRM 53-10-3 FIG 1.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 95FDEA00456Seat Track · brokenINBOARD SEAT TRACK AT POSITION WHERE FWD STANTION ATTACHED TO FLOOR (10L) IS BROKEN. REMOVED AND REPLACED SEAT TRACK AT POSITION WHERE FWD STANTION ATTACHES TO FLOOR (10L) BS 1130 TO 1176 WL 208 LBL 24.75.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00454Seat Track · corrodedCORROSION (72C235-02) ON SEAT TRACK BS 545 TO 560 BL0 WL 208 AND BS 480 TO 494. REMOVE AND REPLACED NEW SEAT TRACK FROM BS 480 TO 600 BL0 WL 208 AS PER FEDEX SRM 53-10-1 AND 53-10-5.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00453Web · crackedCRACK IN LONGITUDINAL WEB BS 850 LBL 45 WL 200. REPAIRED CRACK IN LONGITUDINAL WEB AT BS 850 LBL 45 WL 200 PER FEDEX SRM 51-40-2 AND 51-10-1.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00452Seat Track · corrodedCORROSION ON SEAT TRACK AT BS 620 TO 640 BLO WL 208 HAD MECH DAMAGE AT BS 614. REMOVED AND REPLACED SEAT TRACK FROM BS 600 TO 720 WL 208 BL0.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00451Seat Track · corrodedCORROSION IN THE FWD CARGO BAY IN CARGO SEAT TRACK AT BS 570 LBL 18 WL 156. REMOVED AND REPLACED CARGO SEAT TRACK FROM BS 520 TO 580 LBL 18 WL 156 IN FWD CARGO BAY PER FEDEX SRM 53-10-5.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00450Frame · corrodedCORROSION IN THE FWD CARGO BAY THERE IS CORROSION UNDER FLANGE OF FRAME AT BS 660, RBL 25, WL 156. CORROSION FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1 UNDER FRAME FLANGE AT BS 660 RBL 25 WL 156. REPAIRED FRAME PER FEDEX SRM 57-46-3 AND 53-10-2.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00449Lwr Chord · corrodedCORROSION ON LOWER 740 CHORD AT WL 170, RBL 28. BLENDED AND REMOVED CORROSION ON LOWER 740 CHORD AT WL 170 RBL 28. ORIGINAL THICKNESS OF MATERIAL .0270, REMOVED .083 MATERIAL 1.0 BY 2.0 OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED 740 CHORD PER EA 7-5710-2Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00448Skin · crackedBS 420 TO 440 AT STR 216 TWO POSSIBLE CRACKS IN SKIN. TRIMMED OUT DAMAGED ON SKIN AT STA 430 STR 216, FABRICATED, DRILLED UP, ALODINED, PRIMED, AND INSTALLED DOUBLER AND FILLER. ALL WORK ACCOMPLISHED IAW FEDEX SRM 727-100 (53-30-3) FUNCTIONAL TESTS CHECK GOOApr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA00447Skin · misdrilledDOUBLE HOLE IN SKIN BELOW F/O'S NR 1 WINDOW BS 207 RBL 31 WL 243. REPAIRED DOUBLE HOLE IN SKIN BELOW F/O'S NR 1 WINDOW BS 207 RBL 31 WL 243 IAW FEDEX SRM 53-30-3.Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA00313Actuator · failedAFTER T/O NR 2 SLAT INDICATOR FAILED TO RETRACT. COMPLIED WITH CHECKLIST RETURNED AND LANDED. REPLACED NR 2 L/E SLAT ACTUATOR IAW MM 27-81-32 PG 401-409. SYS OPS NORMAL RII COMPLIED WITH.Mar 17, 1995 · N508FE · Boeing 72725 · Leading Edge Slat ActuatorSDR 95FDEA00216Dnlock Switch · failedON GEAR EXTENSION LEFT MAIN GEAR INDICATED UNSAFE (RED) NOTED A BIRD STRIKE ON LEFT SIDE PRIOR TO GEAR EXTENSION. FOUND LEFT MLG DOWNLOCK SW INOP. REMOVED AND REPLACED LEFT MLG DOWNLOCK SW PER MM 32-61-21 AND 32-61-0 A/C JACKED, GEAR OPS CHECKED NORMAL PER Mar 10, 1995 · N152FE · Boeing 72725 · Landing Gear Position and WarningSDR 95FDEA00174Frame · double drilledDOUBLE HOLE IN FRAME BS 600, STR 4R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 51-40-3.Feb 17, 1995 · N507FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00177Floorbeam · corrodedCORROSION FOUND ON TOP CHORD OF FLOORBEAM BS 276, RBL 12, WL 208. REPAIRED TOP CHORD FLOORBEAM IAW 727 SRM 51-40-04, 51-20-01.Feb 16, 1995 · N507FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00176Floorbeam · corrosionCORROSION ON TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208. REPAIRED TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208 IAW EA 7-5310-23790.Feb 16, 1995 · N507FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00175Floorbeam · corrosionFOUND CORROSION ON FLOORBEAM STA 560, RBL 16, WL 198. REMOVED CORROSION AND REPAIRED FLOORBEAM AT BS 560, RBL 16, WL 198 PER FEDEX EA 7-5310-23795.Feb 16, 1995 · N507FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00173Floorbeam · corrosionCORROSION (72C237-02) UNDER TOP CHORD OF FLOORBEAM AT NUTPLATES HOLES BS 1110, RBL 10-50, WL 208. REPAIRED FLOORBEAM BS 1110, RBL 10-50, WL 208 PER FEDEX EA 7-5310-23793.Feb 16, 1995 · N507FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00149Floor Beam · corrodedCORROSION ON TOP AND BOTTOM OF TOP CHORD OF FLOORBEAM AT BS 344 RBL 17 - LBL 61 WL 208. REPLACED TOP CHORD FROM LBL 707 - RBL 70. IAW FEDEX DRAWING NUMBER SR 27 53-007.Feb 15, 1995 · N507FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00150Shear Tie · crackedFOUND SHEAR TIE CRACKED AT AFT SIDE STA 441 RT BETWEEN STR 18 AND 19, RBL 65. REMOVED CRACKED SHEAR TIE STA 441 RT STR 18 AND 19 (AFT SIDE) RBL 65 AND REPLACED WITH FABRICATED SHEAR TIE.Feb 13, 1995 · N507FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00148Floor Beam · corrodedCORROSION FLOOR BEAM UPPER CHORD BS 680 LBL 36 WL 208. REMOVED CORRODED CHORD, FABRICATED AND INSTALLED REPLACEMENT CHORD AT BS 680 LBL 36 TO RBL 14 WL 208 PER FEDEX SRM 53-10-8.Feb 13, 1995 · N507FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 95FDEA00142Frame · crackedWHILE ACCESSING FOR FUSELAGE 00124, FOUND FRAME CRACKED AT STA 500 RBL 24 WL 158. CUT OUT DAMAGE FRAME AREA. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3.Feb 12, 1995 · N507FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00140Beam · crackedCRACK FOUND ON LONGITUDINAL BEAM AT BS 758 RBL 45 WL 208. REMOVED AND REPLACED LONGITUDINAL BEAM AT STA 758 RBL 45 WL 208.Feb 11, 1995 · N507FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00138Frame · corrodedFOUND CORROSION UNDER NUTPLATE ON FRAME STA 500 LBL 53 WL 175. CUT OUT DAMAGED AREA ON FRAME BS 500 LBL 53 WL 175 AREA OF 1 INCH BY .75 INCH FABRICATED FILLER-DOUBLER AND INSTALLED PER SRM 51-40-3.Feb 11, 1995 · N507FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00141Hinge Fitting · corrodedRIGHT O/B AILERON 2ND HINGE FITTING FROM I/B END HAS CORROSION. REMOVED AND REPLACED NEW AILERON HINGE FITTING.Feb 10, 1995 · N507FE · Boeing 72725 · AileronsSDR 95FDEA00139Frame · corrodedFOUND CORROSION UNDERNEATH NUTPLATE ON FRAME STA 560 LBL 48 WL 170. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.Feb 10, 1995 · N507FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00128Skin · gougedFIXED L/E GOUGED ON LOWER SURFACE AT NR 4 SLAT I/B TRACK. REMOVED EXISTING REPAIR AND FABRICATED AND INSTALLED NEW REPAIR PER FEDEX SRM 5730-2.Feb 9, 1995 · N507FE · Boeing 72725 · Leading Edge DevicesSDR 95FDEA00127Beam · corrodedCORROSION FOUND ON TOP AND BOTTOM SIDE OF LONGITUDINAL BEAM IS SEVERAL AREAS FROM BS 760-840 WL 208 LBL 25. REMOVED AND REPLACED LONGITUDINAL BEAM IAW 53-10-2.Feb 9, 1995 · N507FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA00125Frame · corrodedCORROSION IS FWD CARGO BAY ON FRAME AT BS 520 STR 26 LBL 25. REMOVED CORROSION FROM FRAME OUT OF LIMITS PER SRM REPAIRED PER FEDEX SRM 51-40-3.Feb 9, 1995 · N507FE · Boeing 72725 · Fuselage Main, FrameSDR 95FDEA00123Blkhd Web · crackPOSSIBLE CRACK AT BS 950 BULKHEAD LBL 40 WL 185. REPAIRED CRACK IS 950 BULKHEAD AT LBL 40 WL 185 PER FEDEX SRM 53-10-9 FIG 2.Feb 9, 1995 · N507FE · Boeing 72725 · Fuselage Main, BulkheadSDR 95FDEA00129Doubler · corrodedBS 451-457 BETWEEN STR 18-19R RBL 65 INTERNAL DOUBLER ON E-BAY EXHAUST HAS SIGNS OF CORROSION. REMOVED OLD DOUBLER BS 451-457 STR 18 AND 19R RBL 65 AND INSTALLED NEW DOUBLER.Feb 8, 1995 · N507FE · Boeing 72725 · Fuselage Miscellaneous Structure
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