Boeing 727-25C

Service difficulty reports · 2,007

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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 = '72725C'
  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 UPS205590Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT 930 FRAME CRACKED AT TOP OF FORGED SECTION STR 14 BETWEEN RIVETS ON FACE OF FRAME. REPAIRED RT 930 FRAME AT STR 14R PER UPS EO NR B727-5310-2580-B APPENDIX 8.1 AND 8.2.Feb 22, 1996 · N931UP · Boeing 72725C · Fuselage Main, FrameSDR UPS205595Floorbeam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES STA 680 LBL 60 TO RBL 60, WL 208. CORROSION REMOVAL ON FLOORBEAM UPPER CHORD WAS OUT OF LIMITS PER SRM 53-10-1. BLENDED AREA, FABRICATED REPAIR ANGLES, REPAIRFeb 21, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205593Floorbeam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER CHORD STA 600 RBL 45 TO RBL 65 WL 208, AROUND NUTPLATE HOLES. CORROSION REMOVAL ON UPPER CHORD OF FLOORBEAM WAS OUT OF LIMITS. BLENDED AREA, FABRICATED AND INSTALLED RFeb 21, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205592Floorbeam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES STA 660 RBL 10 TO RBL 55. MECHANICALLY REMOVED CORROSION FROM 660 FLOORBEAM UPPER CHORD RBL 10 TO 58. FOUND REWORK FROM RBL 54 TO 58 TO BE Feb 21, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS2005547Anti-Ice Tube · brokenCREW REPORTED, NR 2 FIRE WARN LIGHT AND BELL WITH CLIMB THRUST, CLIMBING TO ALTITUDE OUT OF ROA. ENGINE NR 2 SHUTDOWN AT 0927Z PER CHECKLIST, FIRE LIGHT WENT OUT AND ALL ENGINE INDICATIONS NORMAL. ENGINE HEAT WAS ON IN THE ICING CONDITIONS. REMOVED AND REPLFeb 21, 1996 · N947UP · Boeing 72725C · Air Intake Anti/De-Ice SystemSDR UPS205582Attach Lug · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 K-FLAP BULLNOSE I/B ROD ATTACH LUG IS CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW UPS OHM 57-51-01.Feb 20, 1996 · N931UP · Boeing 72725C · Leading Edge DevicesSDR UPS205580Stiffener · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER BS 357 LBL 16 AND WL 1498. CORROSION OUT OF LIMITS, REMOVED DAMAGED STIFFENER, FABRICATED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-1 AND DWG-18417.Feb 20, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205579Stiffener · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER BS 358 LBL 6 AND WL 149. CORROSION OUT OF LIMITS, REMOVED DAMAGED STIFFENER, FABRICATED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-1 AND DWG-18417.Feb 20, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205578Mid Chord · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT MID CHORD BETWEEN DOGHOUSE FLOOR AND BS 302 LBL 15 WL 170. CORROSION REMOVED OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED LT MID CHORD IAW SRM 51-30-2, 51-30-4 AND MM 51-20-151.Feb 20, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205576Handle Casting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON RT FWD OVERWING EXIT EXTERIOR HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01.Feb 20, 1996 · N931UP · Boeing 72725C · Emergency ExitsSDR UPS205575Handle Casting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT FWD OVERWING EXIT EXTERIOR HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01.Feb 20, 1996 · N931UP · Boeing 72725C · Emergency ExitsSDR UPS205574Handle Casting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT AFT OVERWING EXIT EXTERNAL HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01.Feb 20, 1996 · N931UP · Boeing 72725C · Emergency ExitsSDR 96FDEA00311Floorbeam · corrodedCABIN FLOORBEAM AT STA 950 IS CORRODED AROUND SCREW HOLES TOP AND BOTTOM OF BEAM FROM SEAT TRACK NR 3 TO NR 5. REMOVED CORROSION PER 51-10-06, OUT OF LIMITS. REPAIRED PER ESO 11782 AND FEDEX EA 7-5310-27477.Feb 20, 1996 · N118FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205573Frame · gougedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR HAS TOOLING MARKS/GOUGES IN Z-FRAME STA 590 WL 302. GOUGE OUT OF LIMITS, FABRICATED REPAIR ANGLE AND HEAT TREATED. INSTALLED PART IAW SRM 51-40-3, 51-10-2, 51-30-2, AND 53-10-1.Feb 19, 1996 · N931UP · Boeing 72725C · Cargo/Baggage DoorsSDR UPS205561Upper Lug · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 K-FLAP O/B UPPER LUG CORRODED AT BONDING POINT. REMOVED AND REPLACED NR 5 K-FLAP IAW UPS MM 27-81-01.Feb 17, 1996 · N931UP · Boeing 72725C · Leading Edge DevicesSDR UPS205566Web · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON WEB AND ANGLES AT STA 203 TO 219 LBL 15 WL 159. REPLACED WEB IAW SRM 51-40-2, 51-30-2, 51-10-6, 51-10-2, 51-10-1, 53-10-1, 51-20-4, AND 51-20-1.Feb 16, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205562Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON I/B CENTER HINGE FITTING AILERON SIDE IS CORRODED AND BEARING BLOCK HAS BLOWN DUST COVER. REPLACED CENTER HINGE FITTING IAW UPS OHM 57-50-111 AND MM 27-10-41.Feb 16, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205560Stiffener · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON VERT STIFFENER AT BS 344 LBL 14 WL 180. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2 AND 51-20-4.Feb 16, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205559Stiffener · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON NOSE GEAR W/W VERT STIFFENER AT BS 344 LBL 14 WL 173 AND 180. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2 AND 51-20-4.Feb 16, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205558Chord · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON MID CHORD BETWEEN DOG HOUSE FLOOR AND CHORD BS 330 AND 346 RBL 15 WL 170. REMOVED AND REPLACED MID CHORD IAW SRM 51-30-2 AND 51-20-4.Feb 16, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205581Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 4 SPOILER HAS AN AREA OF DELAMINATION AROUND CENTER DOUBLER ON THE LOWER SURFACE. REPAIRED NR 4 SPOILER AROUND CENTER DOUBLER IAW SRM 51-40-6 AND 57-50-6.Feb 15, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205577Skin · delaminationWHILE IN FOR C-CHECK, MAINTENANCE REPORTED SPOILER NR 5 HAS DELAMINATION AT THE ACTUATOR FITTING AT FWD EDGE CENTER OF SPOILER BOTH UPPER AND LOWER SURFACE. REPAIRED SPOILER IAW SRM 51-40-6 AND 57-50-6.Feb 15, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205564Seat Track · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION IN WELL OF SEAT TRACK AT STA 680 TO 730, LBL 45, WL 208. REMOVED CORRODED SEAT TRACK FROM BS 650 TO 740, WL 208, LBL 45, FABRICATED NEW SECTION AND INSTALLED. ALL WORK DONE PER SRM 53-10-1 AND 53-10-5.Feb 14, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS205563Seat Track · damagedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, SEAT TRACK STA 480 TO 650 RBL 45 WL 208 HAS MECHANICAL DAMAGE AND CORROSION. REPLACED SECTION OF SEAT TRACK FROM BS 550 TO 650 RBL 45 WL 208. WORK DONE PER SRM 53-10-5 AND 51-30-8.Feb 14, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS205543Center Hinge · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE IS CORRODED AT PANEL ATTACH POINT. REPLACED HINGE FITTING IAW MM 27-10-01.Feb 14, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205542Bullnose · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, L/W NR 2 K-FLAP BULLNOSE IS CORRODED AT O/B HINGE LOWER ATTACH POINT. REMOVED AND REPLACED BULLNOSE IAW MM 27-81-01 AND SRM 57-50-1.Feb 14, 1996 · N931UP · Boeing 72725C · Leading Edge DevicesSDR UPS205536Web · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, VERTICAL WEB FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-2 AT STA 227 LBL 41 TO 44 WL 209 TO 218, CORROSION (C53-221-01,03, 01). REMOVED DAMAGED AREA OF VERTICAL WEB, FABRICATED REPAIR PARTS AND INSTALLED PER 5Feb 14, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205544Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, I/B CENTER HINGE BOLT HOLE CORRODED, NR 3 SPOILER. REMOVED AND REPLACED NR 3 SPOILER ACT HINGE FITTING IAW MM 27-61-81.Feb 13, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205541Spoiler · water entrapedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS POSSIBLE WATER ENTRAPMENT IN VIEW 6 OF X-RAY. REPAIRED NR 1 SPOILER IAW SRM 51-40-6.Feb 13, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205540Spoiler · water entrapedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS POSSIBLE WATER ENTRAPMENT IN VIEW 4 OF X-RAY. REPAIRED NR 1 SPOILER IAW SRM 51-40-6.Feb 13, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205539Skin · delaminationWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS AN AREA OF DELAMINATION AT HINGE AREA FWD EDGE CENTER OF SPOILER UPPER SURFACE. REPAIRED NR 1 SPOILER IAW SRM 51-40-6.Feb 13, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205534Upper Gate · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, MID GALLEY DOOR UPPER GATE HAS AREAS OF CORROSION. REMOVED AND REPLACED MID GALLEY DOOR GATE IAW SRM 51-10-1, 51-20-4, 51-30-8 AND MM 52-12-11.Feb 13, 1996 · N931UP · Boeing 72725C · Galley DoorsSDR 96FDEA00310Bellframe · plugged holeSTR 27L BELLFRAME 990 PLUGGED HOLE TOP NEAR EXISTING FASTENER HOLE. INSTALLED DOUBLER PER SRM 51-40-3.Feb 13, 1996 · N118FE · Boeing 72725C · Fuselage Main, FrameSDR 96FDEA00309Web · corrodedLOWER FUSE CENTER TANK REAR SPAR UPPER CHORD, 3 RIVETS HAD POPPED 2 RIVETS WORKING, SKIN WARP BULGE LBL 18 TO 30. INSTALLED DOUBLER AND TRIPLER TO CENTER TANK UPPER WEB PER ESO 11782 DATED 2-13-96, AWAITING FEDEX EA.Feb 13, 1996 · N118FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205538Skin · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON INSIDE OF FUSELAGE SKIN BELOW FWD TOILET SERVICE PANEL AT BS 300 RBL 54 WL 182. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-30-3 AND 53-30-2.Feb 12, 1996 · N931UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS205535Frame · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED WHILE WORKING NRC 432263 DOOR 74, FOUND THE UPPER FLANGE ON THE LOWER AFT FRAME TO BE CRACKED. REPAIRED UPPER FLANGE ON THE LOWER AFT FRAME ON AFT CARGO DOOR IAW SRM 51-40-3.Feb 12, 1996 · N931UP · Boeing 72725C · Cargo/Baggage DoorsSDR UPS205427Light · inoperativeMAINTENANCE REPORTED, FWD ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD ENTRY LIGHT ASSY, CK NORMAL.Feb 12, 1996 · N933UP · Boeing 72725C · Emergency LightingSDR UPS205599Bulkhead · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED SUSPECTED CRACK AT FASTENER HOLE ON BS 178 BULKHEAD LBL 9, WL 236. REMOVED 2 FASTENERS, CLEANED AREA, NDT INSPECTED FOUND CRACK. TRIMMED OUT AREA THAT WAS CRACKED. NDT VERIFIED CRACK CONTAINMENT FABRICATED REPAIR FFeb 10, 1996 · N931UP · Boeing 72725C · Fuselage Main, BulkheadSDR UPS205537Skin · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON FUSELAGE SKIN AFT OF FWD TOILET SERVICE PANEL BS 310 RBL 68 WL 186. CORROSION OUT OF LIMITS, REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. ALL WORK DONE PER SRM 53-30-3 AND 53-30-2.Feb 10, 1996 · N931UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS205503Seat Track · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK FLANGE AROUND NUTPLATE HOLES AT STA 344-360, LBL 65, WL 208. REPAIRED PER SRM 53-10-1, 51-10-6, 51-30-2, 51-10-2, AND OHM 20-41-02.Feb 10, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS205490Seat Track · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 360-520, RBL 60, WL 208. REPLACED SEAT TRACK PER SRM 51-10-6, 53-10-5, AND 51-30-2.Feb 10, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS205499Stiffeners · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON STIFFENERS AT STA 203, LBL 18 AND 22, WL 180. REPLACED STIFFENERS PER SRM 51-40-4.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205498Intercostal · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 211-219, RBL 25, WL 174. REPLACED INTERCOSTAL PER SRM 53-10-1, 51- 20-1, AND 51-10-22.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205496Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON TAB FITTINGS, TAB SIDE. REPLACED FITTINGS PER SRM 51-30-2.Feb 9, 1996 · N931UP · Boeing 72725C · Aileron TabsSDR UPS205495Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.Feb 9, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205494Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.Feb 9, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205493Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.Feb 9, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205492Floor Beam · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM STA 312, LBL 48, BL ZERO, WL 208, AROUND NUTPLATE HOLES. REPLACED FLOORBEAM PER SRM 53-10-8.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205489Hinge Arm · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION R/W I/B AILERON HINGE ARM. REPLACED HINGE PER UPS MM 27-10-01.Feb 9, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205485Hat Channel · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL AT STA 324-340, RBL 20, WL 208. REPLACED HAT CHANNEL PER SRM 51-20-1, 51-10-2, 51-30-2.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
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