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 UPS205484Stiffener · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION REINFORCING ANGLE AT BS 295, WL 181, RBL 12. REPLACED ANGLE PER SRM 51-10-6, 53-10-6, 53-10-2, 53-10-1, 51-30-5.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205483Stiffener · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON HOR. STIFFENER TOP NOSE WW AROUND FASTENER HEADS BS 308, WL 181, LBL 10, RBL 10. REPAIRED PER SRM 53-10-1, 53-10-2, 51-10-6.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205482Frame · crackedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CRACKED FRAME BS 320, LBL 45. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3.Feb 9, 1996 · N931UP · Boeing 72725C · Fuselage Main, FrameSDR UPS205497Frame · crackedWHILE IN FOR C CHECK, MAINTENANCE REPORTED FRAME CRACKED AT BS 284.5 AT STR 24R, RBL 20. REPAIRED PER SRM 51-30-2 AND 53-10-2.Feb 8, 1996 · N931UP · Boeing 72725C · Fuselage Main, FrameSDR UPS205491Seat Track · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 760-848, RBL 60, WL 208. REPLACED SEAT TRACK PER SRM 51-10-6, 53-10-5, AND 51-30-2.Feb 8, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS205488Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION R/W AILERON O/B HINGE FITTING. REPLACED FITTING PER SRM 51-30-2 AND 51-10-1.Feb 8, 1996 · N931UP · Boeing 72725C · AileronsSDR 96FDEA00308Stiffener · corrodedCENTER TANK STA 870 BL 0 VERTICAL STIFFENER HAS POPPED FASTENERS AND WEB IS BULDGED. INSTALLED NEW CENTER TANK VERTICAL STIFFENER AND WEB REPAIR PER SRM 51-10-1 AND EA 7-5710-27462.Feb 7, 1996 · N118 · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205445Hinge Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE LT I/B AILERON TAB HINGE FITTINGS, AILERON SIDE. REPLACED IAW 727 SRM 51-30-2.Feb 6, 1996 · N931UP · Boeing 72725C · Aileron TabsSDR UPS205444Hinge Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE RT WING I/B AILERON HINGE FITTINGS O/B AND CENTER FITTINGS. REPLACED FITTINGS PER SRM 51-30-2.Feb 6, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205443Hinge · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE RT WING O/B AILERON CENTER O/B HINGE AILERON SIDE. REPLACED PER SRM 51-30-2.Feb 6, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205442Bullnose · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON THE L/W NR 3 K-FLAP BULLNOSE CENTER HINGE LOWER ATTACH POINT. REPLACED NR 3 K-FLAP PER MM 27-81-00.Feb 6, 1996 · N931UP · Boeing 72725C · Leading Edge Slat Control SystemSDR UPS205440Handle · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION OF RT AFT EXTERNAL HANDLE SEAL CASTING ON OVERWING EXIT. REMOVED AND REPLACED CASTING IAW SRM 51-30-02, 51-10-05 AND 51-10-08.Feb 6, 1996 · N931UP · Boeing 72725C · Emergency ExitsSDR 96FDEA00307Stringer · crackedUPPER LOBE MAIN CARGO INTERIOR STRUCTURE, STR 15L CRACKED AT FS 676. REMOVED DAMAGED SECTION OF STR 15L AND INSTALLED STR SPLICE REPAIR PER SRM 53-10-3 FIG 1 PG 3 TO 48.Feb 6, 1996 · N118FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR UPS205400Hinge Fitting · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON O/B HINGE FITTING IS CORRODED. REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-30-2.Feb 5, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS96205648Chord · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INNER CHORD FIN STA 22.5 IS CRACKED. REMOVED DAMAGED AREA I.A.W. BOEING DWG 65C20296. INSTALLED REPAIR DOUBLER PER BOEING DWG 65C20296 AND SRM 51-30-2.Feb 4, 1996 · N949UP · Boeing 72725C · Vertical StabilizerSDR UPS205401Hinge Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER O/B HINGE FITTING IS CORRODED. REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-30-2.Feb 4, 1996 · N931UP · Boeing 72725C · AileronsSDR UPS205441Thrust Shaft · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON THE NR 7 FLAP CARRIAGE LOCATER ON THE THRUST SHAFT FWD OF THE THRUST NUT. RECEIVED NEW FLAP CARRIAGE.Feb 3, 1996 · N931UP · Boeing 72725C · Trailing Edge FlapsSDR UPS205399Angle · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON WEB TIE ANGLE AT STA 804 STR 10 RT. REPAIRED WEB AND FABRICATED TIE ANGLE.Feb 3, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205565Support Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, FLUORESCENT PENETRANT INSPECTION OF THE NR 11 O/B FLT SPOILER ACT SUPPORT FITTING, EXHIBITS CORROSION INDICATIONS AROUND THE HOLE ON BOTH THE I/B AND O/B LOWER LUGS. REMOVED AND INSTALLED NEW FITTING. WORK DONE PER Feb 2, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205501Spoiler · water entrapmentWHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW X-RAY NR 3 SPOILER. REPAIRED PER SRM 51-40-6.Feb 2, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205439Shear Tie · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED UPPER SHEAR TIE CRACKED AT BS 277, STR 16 RT, ACCESSING REQ. REPAIRED IAW 51-40-02 FIG 1.Feb 2, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205507Spoiler · water entrapmentWHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 5 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6.Feb 1, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205506Spoiler · water entrapmentWHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 4 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6.Feb 1, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205505Spoiler · water entrapmentWHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 6 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6.Feb 1, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205504Spoiler · water entrapmentWHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 8 OF X-RAY OF SPOILER NR 9. REPAIRED PER SRM 57-50-6.Feb 1, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205502Spoiler · water entrapmentWHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 5 X-RAY NR 7 SPOILER. REPAIRED PER SRM 51-40-6.Feb 1, 1996 · N931UP · Boeing 72725C · SpoilersSDR UPS205583Seat Track · damagedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MECHANICAL DAMAGE ON SEAT TRACK AT STATION 680 TO 700 LBL 65 WL 208. FOUND DAMAGE TO BE OUT OF LIMITS, REMOVED DAMAGED SEAT TRACK AND REINSTALLED FABRICATED SEAT TRACK WITH FASTENERS AT STA 683 TO 740 IAW SRM 51-30-0Jan 31, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS205600Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT STA 930 FRAME CRACKED ON ZEE FRAME T-FORGED FRAME AT SPLICE ON STRINGER NR 14. REMOVED CRACKED FRAME, POSITIONED AND INSTALLED NEW FRAME, LOCATED ALL HOLES AND SECURED WITH FASTENERS IAW EO B747-5310-2580-B ER 020Jan 29, 1996 · N931UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96205645Skin · gougedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED SKIN PANEL STA 1243-1342, STR 11L-14L HAS GOUGE. REMOVED SKIN, FABRICATED AND INSTALLED STRINGER PER BOEING DWG 65-17528 AND SRM 51-30-2.Jan 28, 1996 · N949UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS96205644Skin · gougedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED SKIN PANEL STA 1243-1342, STR 11R-14R HAS GOUGE. REMOVED SKIN, FABRICATED, AND INSTALLED STRINGER PER BOEING DWG 65-17558 AND SRM 51-30-2.Jan 28, 1996 · N949UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR 96FDEA00116Valve · damagedBOTH LT AND RT PURGE SHUTOFF VALVES PHYSICALLY DAMAGED, ENDS BLOWN OFF. REMOVED AND REPLACED VALVES, LT-12231, RT-C64198.Jan 23, 1996 · N116FE · Boeing 72725C · Pneumatic Distribution SystemSDR UPS96205649Spar Chord · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INBOARD MID-FLAP WBL 124.2 REAR SPAR 4TH FASTENER HOLE REVEALED A CRACK ON SPAR CAP BELOW SKIN AT 3 O'CLOCK POSITION. LOWER PANEL WAS OPENED, 10 EACH FASTENERS REMOVED. REPAIRED HOLE AREA I.A.W. DHC SK 949-436 AJan 19, 1996 · N949UP · Boeing 72725C · Trailing Edge FlapsSDR UPS96205647Window Frame · corrosionWHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT WINDOW FRAME FS 530 AFTER CORROSION REMOVAL, FLANGE FOUND BEYOND LIMITS PER SRM 56-20-1 ON NR 408505. FABRICATED DOUBLER AND INSTALLED CONICAL WASHERS PER SRM 56-20-3, FIG 1. INSTALLED REPAIR DOUBLER PER SRM 56-Jan 19, 1996 · N949UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96205646Window Frame · corrosionWHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT WINDOW FRAME FS 590 AFTER CORROSION REMOVAL. LOWER FLANGE FOUND BEYOND LIMITS PER SRM 56-20-1 ON NR 408510. FABRICATED DOUBLER AND INSTALLED CONICAL WASHERS PER SRM 56-20-3, FIG. 1. INSTALLED REPAIR DOUBLER PERJan 19, 1996 · N949UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96205641Spar · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED FS 1342, THE VERTICAL FIN REAR SPAR CHORD CRACKED. REPAIRED I.A.W. BOEING DWG 69-70556.Jan 17, 1996 · N949UP · Boeing 72725C · Vertical Stabilizer, Spar/RibSDR UPS96205660Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT SKIN SUPPORT ANGLE CRACKED FS 1345 FIN STA 22.5. REMOVED, FABRICATED AND INSTALLED NEW ANGLE SECTION IAW SRM 51-40-3 AND 51-30-2.Jan 10, 1996 · N949UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96205642Rib · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT RIB CRACKED BS 1367 FIN STA 22.5. CUT OUT DAMAGE AND REPAIRED WEB I.A.W. SRM 51-40-2.Jan 10, 1996 · N949UP · Boeing 72725C · Vertical Stabilizer, Spar/RibSDR UPS205486Floor Beam · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 344, RBL 17-20, WL 208. REPAIRED FLOOR BEAM PER SRM 53-10-8, FIG. 7 AND E.R. NR 020696CD3, 53-10-10.Jan 9, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96205643Stringer · corrosionWHILE IN FOR MOD WORK, MAINTENANCE REPORTED STR 26L AT BS 294.5 HAS HEAVY CORROSION. INSTALLED REPLACEMENT ANGLE PER SRM 51-30-2 AND SRM 53-10-2.Jan 4, 1996 · N949UP · Boeing 72725C · Fuselage Main, Longeron/StringerSDR UPS205148Battery · dischargedMAINTENANCE REPORTED, DURING WEEKEND CHECK EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND OPS CHECK GOOD.Dec 16, 1995 · N937UP · Boeing 72725C · Emergency LightingSDR UPS205116Battery · dischargedWHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPAIRED BATTERY (BOTH) EMERGENCY LIGHTS. OPS CHECK O.K.Nov 30, 1995 · N937UP · Boeing 72725C · Emergency LightingSDR UPS205118Battery · dischargedWHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHTS WILL NOT ILLUMIATE. REPLACED BATTERY. OP CHECK GOOD.Nov 29, 1995 · N937UP · Boeing 72725C · Emergency LightingSDR UPS205105Battery · dischargedWHILE ON GROUND, MAINT FOUND FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BOTH EMERGENCY LIGHT BATTERIES, OPS CHECK OK.Nov 20, 1995 · N937UP · Boeing 72725C · Emergency LightingSDR 95FDEA01753Fitting · corrodedLT STA 740 WING TERMINAL FITTING ON FUSELAGE, BORE IS CORRODED. REMOVED CORROSION BY BORING HOLE TO 3500 PER SRM 57-10-7 PAGE 3, MADE SLEEVE PER SRM 57-10-7 PART 9 AND 10. INSTALLED TERMINAL SLEEVE PER SRM 51-10-1.Nov 14, 1995 · N133FE · Boeing 72725C · Wing Miscellaneous StructureSDR 95FDEA01722Floorbeam · corrodedSTA 380 FLOORBEAM FOUND TO BE TOO THIN AFTER CORROSION REWORK AT APPROX LBL 54 UPPER AFT FLANGE. REPAIRED FLOORBEAM PER EA 7-5310-25983 DATED 10-26-95.Nov 13, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01723Trunnion · crackedL/W FRONT SPAR BOTTLE BOLT TRUNNION FS 740 CRACKED INSIDE PIN HOLE, 3 PLACES. REMOVED AND REPLACED TRUNNION IAW BOEING DRAWING NR 65C29064.Nov 9, 1995 · N133FE · Boeing 72725C · Wing, Landing Gear Attach FittingsSDR UPS204949Wing Tip · crackedWHILE ON GROUND, MAINTENANCE FOUND RT WING TIP LWR SURFACE HAS TWO, 6 INCH CRACKS. C/W TEMPORARY REPAIR OF RT WING TIP LOWER SURFACE PER EO B727-5730-7604-A.Nov 7, 1995 · N915UP · Boeing 72725C · Wing Miscellaneous StructureSDR UPS204948Battery · dischargedWHILE ON GROUND, MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED N1-CAD BATTERIES, OPS CHECK GOOD.Nov 7, 1995 · N937UP · Boeing 72725C · Emergency LightingSDR UPS204935Eel Assy · inoperativeWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT WOULD NOT TEST DURING PREFLIGHT. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY.Nov 2, 1995 · N932UP · Boeing 72725C · Emergency LightingSDR 95FDEA01637Floor Beam · corrodedMAIN CARGO - CORROSION ON BOTTOM OF UPPER FLANGE OF FLOOR BEAM AT STA 640 BETWEEN NR 5 AND NR 6 SEAT TRACK. REMOVED CORROSION PER SRM 51-10-06. REPAIRED FLOOR BEAM PER ESO 11782 AND FEDEX EA 7-5310-25944.Oct 30, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor Beam
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