Boeing 727-31C

Service difficulty reports · 885

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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 = '72731C'
  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 UPS99228958Structure · crackedINSPECTION TYPE-D, A NUMBER OF CRACKS FOUND ON AFT CARGO DOOR STRUCTURE. DOOR REPLACED IAW MM 52-31-00.Feb 11, 1998 · N923UP · Boeing 72731C · Cargo/Baggage DoorsSDR UPS98225392Rudder · splitDURING EACH LEG, THE RUDDER TRIES TO SPLIT AT VARIOUS SPEEDS AND ALTITUDES. INSPECTED RUDDER SYSTEM FOR LOOSE TABS OR COMPONENTS, NONE FOUND. COULD NOT DUPLICATE ON GROUND, ALL WORK DONE IAW MM 27-20 AND 27-30-143. NO FAULTS NOTED. ALL OPS CHECKS NORMAL, AJan 7, 1998 · N922UP · Boeing 72731C · Rudder Control SystemSDR UPS97224679Skin · corrodedCORROSION DAMAGE JUST FWD OF L1 DOOR APPROX 12 IN EXT SKIN 5X 2 REF DMI 140558. REMOVED AND REPLACED LEFT SIDE FUSELAGE SKIN PANEL FROM STA 259.5 TO STA 312 AND S-10L TO S-14L AS PER UPS EO B727-5330-9847-A DATED 10/31/97. (REF N/R 731755).Oct 13, 1997 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS97224002Frame · damagedINSPECTION TYPE-C, FRAME AT BS 848.95 RT HAS DAMAGE TO FASTENER HOLE, SECOND FASTENER HOLE ABOVE FLOOR LINE. REPAIR CARRIED OUT IAW SRS EO 97-17-009, UPS APPROVAL NUMBER 727-53- 1953.Aug 5, 1997 · N923UP · Boeing 72731C · Fuselage Main, FrameSDR UPS97223994Pressure Floor · crackedINSPECTION TYPE-C, 2 CRACKS IN MLG PRESS FLOOR LT WHEEL WELL BS 920 TO 930 LBL 0 TO 17. REPAIR CARRIED OUT IAW EO B727-5310-0088.Aug 1, 1997 · N923UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97224006Frame · damagedINSPECTION TYPE-C, FRAME AT BS 825.95 RT HAS DAMAGE TO FASTENER HOLE ABOVE FLOOR LINE, SECOND FASTENER HOLE ABOVE FLOOR LINE. REPAIR CARRIED OUT PER SRS EO 97-17-008, UPS APPROVAL NUMBER 727-53- 1952.Jul 29, 1997 · N923UP · Boeing 72731C · Fuselage Main, FrameSDR UPS97224003Engine Mount · corrodedINSPECTION TYPE-C, PITTING CORROSION IN FWD OUTBOARD BOLT HOLE ON NUMBER 1 ENGINE FWD MOUNT FITTING. REPAIR CARRIED OUT PER SRS EO 97-17-001 AND 97-17-003, UPS APPROVAL NUMBER 727-71-051.Jul 28, 1997 · N923UP · Boeing 72731C · Engine Mount SectionSDR UPS97223975Angle · crackedINSPECTION TYPE:C, BS 950 RT FITTING LWR INBOARD HORIZONTAL SUPPORT ANGLE FOUND CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-30-2 AND DWG NR 65C18332.Jul 28, 1997 · N923UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97223995Fitting · crackedINSPECTION TYPE:C, INBOARD SPOILER SUPPORT ATTACH FITTING FOR NR 6 FLAP TRACK CRACKED. FITTING REPLACED IAW SRM 51-30-2.Jul 27, 1997 · N923UP · Boeing 72731C · Wing, Control Surface Attach FittingsSDR UPS97224001Str Vent Tab · crackedINSPECTION TYPE-C, RT WS 629.0 STR 14 VENT FWD TAB IS CRACKED. ALSO, STR 13 IS CRACKED. CRACKS IN TABS AT STR 14 AND STR 13 STOP DRILLED IAW EO B727-5710-0 314 APP 8.3, REPAIR CARRIED OUT IAW EO B727-5710-0314 APP 8.3Jul 25, 1997 · N923UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS97223976Skin · crackedINSPECTION TYPE:C, LT WING GEAR DOOR SKIN AT AFT HINGE AREA CRACKED. REPAIRED IAW EO B727-5280-4505-A.Jul 23, 1997 · N923UP · Boeing 72731C · Landing Gear DoorsSDR UPS97224004Stringer · crackedINSPECTION TYPE-C, SUSPECT CRACK IN STRINGER 26R JUST FORWARD OF FRAME 360. SUSPECT CRACK IS PROPOGATING FROM END FASTENER HOLE IN STRINGER. REPAIR CARRIED OUT IAW SRM 53-10-3 FIGURE 2.Jul 21, 1997 · N923UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS97224000Frame · damagedINSPECTION TYPE-C, FASTENER HOLE DAMAGE IN FRAME BS 783.95 RT. SECOND FASTENER HOLE ABOVE FLOOR LINE. REPAIR CARRIED OUT IAW SRS EO 97-17-007, UPS EO B727-5310-9619-A.Jul 21, 1997 · N923UP · Boeing 72731C · Fuselage Main, FrameSDR UPS97223997Seat Track · crackedINSPECTION TYPE-C, SEAT TRACK SECTION CORRODED AND CRACKED BS 344 TO BS 390 LBL 24.75. SEAT TRACK SECTION BS 390 TO BS 344 LBL 24.75 REPLACED IAW SRM 53-10-5.Jul 21, 1997 · N923UP · Boeing 72731C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97223993Tail Cone · delaminatedINSPECTION TYPE:C AREA OF DELAMINATION LEFT AFT SIDE OF TAIL CONE REPLACMENT CONE FITTED IAW MM 55-30-21Jul 20, 1997 · N923UP · Boeing 72731C · Aerodynamic FairingsSDR UPS97224005Fitting · crackedINSPECTION TYPE-C, TWO CRACKS FOUND ON BS 950 SIDE FITTING, RT BETWEEN STRINGER 10 AND STRINGER 11, ON OUTER FLANGE, FWD RADIUS. CRACK NR 1 IS 3.5 INCHES LONG, CRACK NR 2 IS 1 INCH LONG. BS 950 FITTING REPLACED IAW UPS ENGINEERING ORDER B727-5310-3012, BOEIJul 18, 1997 · N923UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97223979Frame · corrodedINSPECTION TYPE:C, CORROSION ON GALLEY FLOOR SUPPORT FRAME STN 340 RBL 35. SUPPORT FRAME FABRICATED AND FITTED IAW SRM 51-30-2.Jul 17, 1997 · N923UP · Boeing 72731C · Fuselage Main, FrameSDR UPS97223982Intercostal · corrodedINSPECTION TYPE:C, CORROSION IN INTERCOSTAL UNDER COCKPIT DOOR. INTERCOSTAL FABRICATED IAW 51-20-1 FITTED IAW 51-30-2.Jul 16, 1997 · N923UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97223980Frame · corrodedINSPECTION TYPE:C, SURFACE CORROSION ON FWD TOILET SILL SUPPORT FRAME BS 310 TO 350 RBL 16. SILL FABRICATED AND FITTED REF SRM 51-30-2.Jul 16, 1997 · N923UP · Boeing 72731C · Fuselage Main, FrameSDR UPS97223981Floorbeam · corrodedINSPECTION TYPE:C, SURFACE CORROSION ON FLOORBEAM BS 344 RBL 12 LBL 24. FLOORBEAM TOP CHORD FABRICATED AND INSTALLED REF BOEING DWG NR 65-16 316.Jul 14, 1997 · N923UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS97222159Flap · corrodedINSPECTION TYPE-C, CORROSION ON NR 4 KREUGER FLAP FOUND TO BE BEYOND LIMITS OF SRM 57-50-1. KREUGER FLAP REPLACED IAW MM 27-81-01.Feb 24, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222158Flap · corrodedINSPECTION TYPE-C, NR 5 KREUGER FLAP CORRODED BEYOND SRM 57-50-1 LIMITS. NR 5 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.Feb 24, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222157Flap · corrodedINSPECTION TYPE-C, NR 6 KREUGER FLAP CORRODED BEYOND LIMITS OF SRM. NR 6 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.Feb 24, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222117Skin · crackedINSPECTION TYPE-D, LT WING LE SLAT NR 3 CRACK AT RIVET HOLE ON LE SKIN CENTER. *S/D* HFEC INSPECTED PER NDT PT6 51-00-00 FIG4, CRACKS CONTAINED BY STOP DRILL HOLES. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 1.Feb 14, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222089Fitting · corrodedINSPECTION TYPE-C, STR 22 LT END FITTING CORRODED BS 360. *S/D* STRINGER END FITTING REPLACED IAW BOEING DRAWING 65-18420.Feb 14, 1997 · N927UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97222156Flap · corrodedINSPECTION TYPE-C, WIDE SPREAD PITTING CORROSION ON NR 2 KREUGER FLAP. CORROSION BEYOND REPAIRABLE LIMITS OF SRM 57-50-1. NR 2 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.Feb 12, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222126Rib · crackedINSPECTION TYPE-D, SLAT 5 CRACK ON RIB AT WS 464 SLAT STA 120. CRACK APPROX .75 INCH LONG. *S/D* HFEC CARRIED OUT IAW NDT PT 6 51-00-00 FIG 4. CRACK FOUND TO BE CONTAINED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 9.Feb 12, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222125Panel · corrodedINSPECTION TYPE-D, PANEL ON UNDERSIDE OF WALKING BEAM IN RT MAIN LANDING GEAR WHEEL WELL HAS SOME SURFACE CORROSION. *S/D* CORROSION FOUND TO BE OUTSIDE LIMITS PER SRM 51-10-01. PANEL REPLACED IAW SRM 51-30-2.Feb 12, 1997 · N927UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97222124Stringer · crackedINSPECTION TYPE-D, LT WING CRACK ON VENT STRINGER TAB NR 14 AT WS 686.5. *S/D* CRACKED TAB REMOVED PER SRM 51-10-6. HFEC CARRIED OUT IAW NDT PT 6 5 1-00-00 FIG 4, NO DEFECTS INDICATED. REPAIR CARRIED OUT IAW SB 727- 57A0159 FIGS 2 AND 4.Feb 12, 1997 · N927UP · Boeing 72731C · Wing, Longeron/StringerSDR UPS97222122Hinge Fitting · corrodedINSPECTION TYPE-D, RT O/B AILERON NR 2 HINGE FITTING CASTING SHOWS SIGNS OF CORROSION. FITTING REPLACED IAW SRM 51-30-2.Feb 12, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222121Bracket · corrodedINSPECTION TYPE-C, RT INBAORD AILERON TURNAROUND PULLEY SUPPORT CASTING HAS CORROSION. ALSO, PLAY ON PULLEY (TURNAROUND PULLEY). *S/D* CASTING REPLACED IAW SRM 51-30-2. PLAY REMOVED BY BEARING REPLACEMENT PER MM 20-10-07.Feb 12, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222116Casting · corrodedINSPECTION TYPE-D, ON REMOVAL OF AILERON CONTROL TURNAROUND PULLEY, BRACKET MOUNTING PULLEY FOUND TO BE SEVERELY CORRODED. *S/D* CASTING REPLACED IAW SRM 51-30-02.Feb 12, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222115Skin · corrodedINSPECTION TYPE-D, SUSPECT 10 TO 15 PERCENT MATERIAL LOSS BETWEEN S6R-S7R ON FWD SKIN AT BS 481 BUTT JOINT. *S/D* REPAIR CARRIED OUT IAW B727-5310-1371 APPENDIX 8.5.Feb 12, 1997 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS97222114Skin · corrodedINSPECTION TYPE-D, SUSPECT 10 TO 15 PERCENT MATERIAL LOSS FROM JUST ABOVE S9R TO JUST ABOVE S10R AT BS 481 BUTT JOINT. *S/D* REPAIR CARRIED OUT IAW EO B727-531-1371 APPENDIX 8.5.Feb 12, 1997 · N927UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS97222091Casting · corrodedINSPECTION TYPE-C, RT I/B AILERON TAB O/B BEARING CASTING SHOWS SIGNS OF CORROSION. *S/D* FITTING REPLACED IAW SRM 51-30-2.Feb 12, 1997 · N927UP · Boeing 72731C · Aileron TabsSDR UPS97222090Support · corrodedINSPECTION TYPE-C, NR 3 FLAP TRANSMISSION SUPPORT FITTING CORRODED IN MOUNTING HOLES FOR TRANSMISSION. *S/D* FLAP TRANSMISSION SUPPORT FITTING REPLACED IAW SRM 51-30-02.Feb 12, 1997 · N927UP · Boeing 72731C · Trailing Edge FlapsSDR UPS97222088Casting · corrodedINSPECTION C-CHECK, RT INBOARD AILERON TURNAROUND PULLEY SUPPORT CASTING HAS CORROSION. CASTING REPLACED IAW SRM 51-30-2.Feb 12, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222120Hinge Fitting · corrodedINSPECTION TYPE-C, LT OUTBOARD AILERON HINGE FITTING 4TH HINGE OUTBOARD CORRODED IN BUSH HOUSING. *S/D* FITTING REPLACED IAW BOEING DRAWING 65-19277.Feb 11, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222119Fitting · crackedINSPECTION TYPE-C, ON INSPECTION OF BS 740 FITTING LT, CRACK AT LWR FASTENER HOLE FOUND TO BE PROGRESSED FROM LOWER FASTENER TO END OF FITTING. *S/D* HFEC INSPECTION CARRIED OUT IAW NDT PT6 51-00-00 FIG 4. CRACK FOUND TO HAVE PROGRESSED FROM LOWER FASTENER Feb 11, 1997 · N927UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97222113Fitting · corrodedINSPECTION TYPE-D, LT OUTBOARD AILERON HINGE FITTING 2ND HINGE OUTBOARD CORRODED IN BUSHING AREA. FITTING REPLACED IAW DWG 65-19275.Feb 11, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222112Stringer · corrodedINSPECTION TYPE-D, INVESTIGATE EVIDENCE OF CORROSION ON STRINGER 26R BS 520. *S/D* STRINGER FOUND CORRODED BEYOND LIMITS PER SRM 51-10-6. STRINGER REPLACED IAW SRM 51-10-1 AND 51-30-2.Feb 11, 1997 · N927UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS97222111Angle · crackedINSPECTION TYPE-D, ON REMOVAL OF SKIN PANEL FRAME ATTACH ANGLE BS 328 BETWEEN S18L AND S19L FOUND CRACKED. *S/D* CRACK STOP TRIMMED, HFEC CONFIRMED PER NDT PT6 51-00-00 FIG 4. REPAIR CARRIED OUT IAW SRS EO 97-01-002 (UPS MINOR REPAIR AUTHORISATION FILE NO 7Feb 11, 1997 · N927UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97222136Skin · corrodedINSPECTION TYPE-C, NR 1 KREUGER FLAP CORRODED CORROSION BEYOND LIMITS PER SRM 57-50-1. KREUGER FLAP REPLACED IAW MM 27-81-01.Feb 10, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222134Fitting · crackedINSPECTION TYPE-C, NR 14 SPOILER O/B CASTING SECURING SPOILER PANEL STOP IS CRACKED. CASTING REPLACED IAW SRM 51-30-02.Feb 10, 1997 · N927UP · Boeing 72731C · SpoilersSDR UPS97222110Arm Support · corrodedINSPECTION TYPE-D, LT INBOARD AILERON MIDDLE HINGE SUPPORT ARM CORRODED. *S/D* AILERON MIDDLE HINGE SUPPORT ARM REPLACED IAW MM 27-10-01.Feb 10, 1997 · N927UP · Boeing 72731C · AileronsSDR UPS97222092Support · corrodedINSPECTION TYPE-C, AREA UNDER LAVATORY, CORROSION ON TOP-HAT SECTION AT LAVATORY ENTRY THRESHOLD AT BS 348.2 RBL 24.75. *S/D* NEW SECTION OF SUPPORT FABRICATED FROM EXTRUSION BAC 1510-335 AND FITTED IAW SRM 51-30-2.Feb 9, 1997 · N927UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS97222118Skin · damagedINSPECTION TYPE-C, REF STAR AIR NRC 235558 : TEMPORARY REPAIR CARRIED OUT TO LT OUTBOARD MID FLAP TRAILING EDGE INBOARD SIDE UPPER SKIN. *S/D* TEMPORARY REPAIR REMOVED AND PERMANENT REPAIR CARRIED OUT IAW SRM 51-4 0-6 FIG 25. FOKKER BOND TEST CARRIED OUT IAFeb 7, 1997 · N927UP · Boeing 72731C · Trailing Edge FlapsSDR UPS97222109Skin · crackedINSPECTION TYPE-D, OUTER SKIN ON LOWER SURFACE OF NR 5 SLAT OUTBOARD END CRACKED APPROX 6 CM. HFEC INSPECTED PER NDT PT6 51-00-00 FIG 4, CRACK CONTAINED BY FASTENER HOLE AND STOP DRILL HOLE. REPAIR CARRIED OUT PER SRM 57-30-3 FIG 1.Feb 7, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222135Skin · corrodedINSPECTION TYPE-C, PAINT BLISTERING FROM NR 3 KREUGER FLAP. SUSPECT CORROSION ON INVESTIGATION CORROSION FOUND TO BE OUTSIDE. REPAIR LIMITS OF SRM 57-50-1. NR 3 KREUGER FLAP REPLACED IAW MM 27-81-01.Feb 6, 1997 · N927UP · Boeing 72731C · Leading Edge DevicesSDR UPS97222127Skin · corrodedINSPECTION TYPE-C, SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL STRUCTURE AT BS 348 AND 312 BETWEEN S19 AND 20 LT. *S/D* NDT INSPECTION CARRIED OUT PER NDT PT 6 51-00-00 FIG 5, 20 PERCENT LOSS OF MATERIAL INDICATED.Feb 6, 1997 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
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