Boeing 727-232
Service difficulty reports · 6,539
Newest first. General aviation reporting is voluntary.
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 = '727232' 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.
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 = '727232' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA9800630Floorbeam · corrodedINSPECTION FOUND LOWER CAP OF FLOORBEAM CORRODED AT FS 1070 FROM LBL 39 TO RBL 48. THE LOWER CAP WAS CUT OUT, L-ANGLES, FILLER AND A STRAP WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 8.SDR CALA9800628Floorbeam · corrodedINSPECTION FOUND LOWER CHORD OF FLOORBEAM CORRODED AT STA 1130, RBL 0 TO RBL 60. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03707.SDR DL72S980808Angle · corrosionDURING MV1 CHECK TASK C53-113-01, CORROSION FOUND ON SKIN SUPPORT ANGLE AT STA 740 STR 27R. REPLACED SUPPORT ANGLE PER M/M 53-11-0 PG 858.SDR CALA9800627Skin · corrodedINSPECTION FOUND SCREW HOLE ON TOP OF LT WING FIXED LEADING EDGE CORRODED AT WS 250. THE CORROSION WAS REMOVED IAW SRM 57-20-1. THE CORRODED AREA OF SKIN WAS CUT OUT. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW AEROCORP ENGINEERING ORDER 04884.SDR 98FDEA00232Rib · crackedRIB CRACKED AT BS 1283 AT 7 O'CLOCK POSITION ON S-DUCT. *S/D* REPAIRED RIB AT BS 1283 AT 7 O'CLOCK POSITION ON 5 DUCT IAW FED-EX SRM 54-10-3.SDR DL72S980771Spar · misdrilledNR 3 MIDFLAP/ REAR SPAR/WBL 124/AD 94-07-08 - OS HOLE: OVERSIZED HOLE IN REAR SPAR UPR CHORD AND UPPER SKIN IN AD INSPECTION AREA. FOUND DURING ACCOMPLISHMENT OF EO, 4-58705-3AD MODIFICATION. FAA AMOC REC'D TO INSTALL OS HI-LOK IN HOLE.SDR DL72S980755Bear Strap · crackedTHE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER THE DIRECTION OF BAC S/B 727-53-0136 AND ER/A 364433-14.SDR DL72K980722Battery · dischargedCARGO DOOR EMERGENCY LIGHT BATTERY PACK FAILED ON TEST. REPLACED BATTERY PACK.SDR DL72S980796Skin · crackedDURING INSPECTION OF FWD SVC DOOR UPPER HINGE CUTOUT REF SI 4-72762-12 ME 02, .25 INCH VISIBLE CRACK FOUND IN BEAR STRAP. REPAIRED PER ER/A 364433-14 CODE 4-53-31-20.SDR DL72S980690Bracket · crackedFOUND ON D1 LETTER CK, NR 2 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER RADIUS. REPAIRED PER MM 57-20-21.SDR DL72S980689Web · crackedFOUND ON D1 LETTER CK, LT VERT TORQUE BOX WEB CRACKED AT UPPER END AT STA 1237 LT. REPAIRED PER MM 53-11-0.SDR CALA9800696Support · crackedINSPECTION FOUND CRACKS IN FORWARD PIT FLOOR SUPPORT AT STA 714, LBL 2. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1, PAGE 6. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-3.SDR CALA9800606Skin · dentedINSPECTION FOUND A DENT IN LT WING LEADING EDGE NR 1 SLAT. THE DENTED AREA WAS REMOVED. THE AREA WAS REINFORCED WITH A NEW DOUBLER WHICH WAS FABRICATED AND INSTALLED IAW SRM 57-10-00 FIGURE 18A 51-20-00 AND 51-31-01.SDR CALA9800604Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 480, RBL 48. A SEAT TRACK REPAIR WAS FABRICATED AND INSTALLED IAW 53-10-5, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800603Bulkhead · crackedINSPECTION FOUND A 3 INCH CRACK AROUND FASTENERS ON STA 1183 BULKHEAD AT RBL 7, WL 192 ABOVE TAIL SKID AT SECOND ANGLE FROM TOP. THE CRACK WAS ROUTED OUT IAW ECRA 5310-01473. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01473, SRM 51-30-2, AND 51-10-SDR CALA9800602Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK ON AFT SIDE OF STA 1183 BULKHEAD AT RBL 7, WL 192 JUST ABOVE TAIL SKID ATTACH UPPER L-ANGLE TO LOWER L-ANGLE. THE CRACK WAS ROUTED OUT IAW ECRA 5310-01473. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01473, SRM 51-30-SDR DL72S980697Bushing · wornLT HORIZ STAB NR 1 HINGE ATT PT FUS ELEV, FITTING AND BUSHINGS ARE WORN. SPOTFACE I/B FACE OF O/B LUG .012 REMOVED BUSHINGS, CLEANED LUG WITHIN LIMITS PER MM 55-50-0 FIG 801. ROTOPEENED PER PS900-4 TREAT FACES AND BORES. PAINTED FACES AND BORES. TURNED BUSSDR DL72K980675Accessory Unit · failedWHEN GEAR HANDLE SELECTED DOWN GEAR LIGHTS DID NOT ILLUM. GEAR HANDLE WAS SELECTED UP BUT WOULD NOT GO PAST OFF. POM ABNML PROCEDURE WAS C/W. FOUND LEVER LATCH CB POPPED. RESET CB GEAR, LIGHTS ILLUMINATED, GEAR WAS VISUALLY CONFIRMED DOWN. FOUND LEVER LATSDR CALA9800600Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 480, RBL 48. THE CORRODED AREA WAS REMOVED, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 1.SDR DL72S980809Blkhd Angle · crackedDURING MV1 CHECK, FOUND KEEL BEAM SUPPORT ANGLE CRACKED 3.5 INCHES, FWD SIDE OF STA 870 BULKHEAD, RT SIDE OF KEEL BEAM. REPLACED ANGLE PER SRM 53-10-9 FIG 13.SDR DL72S980775Doubler · crackedAFT SPAR CHORD DOULBER CRACKED TWO PLACES 34 FROM I/B END OF NR 3 MIDFLAP. REPLACED DOULBER PER BOEING M/M 57-52-0 FIG 802. .SDR DL72S980673Indicator · shortedAT FL 310 HAD STRONG ELECT SMELL LIKE PLASTIC BURNING. INDICATOR LTS MASTER SECT 1 C/B POPPED. ODOR SLOWLY SUBSIDED, FOUND COCKPIT INDICATOR SHORTING TO GROUND. REPOSITIONED TERMINALS, CKS OK.SDR CALA9800599Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 440 TO 480, RBL 24. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-10-5, 53-10-5, 51-30-5, 51-30-8, 51-10-2, 51-30-2 AND MM 51-20-11.SDR CALA9800598Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1070 TO 1050, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, 51-30-5, AND MM 51-20-0.SDR CALA9800597Support · corrodedINSPECTION FOUND AFT LAV LT SUB FLOOR SUPPORT CORRODED AT STA 1130 TO 1170, LBL 25 TO 60. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW FLOOR SUPPORT PANEL WAS FABRICATED AND INSTALLED.SDR DL72S981448Angle · crackedLOWER AFT CHORD ANGLE IS CRACKED AT 19, 22, 32, 37, 54 AND 59 FORM I/B END OF FLAP. REPAIR PER M/M 57/52/0 FIG 802.SDR DL72S980829Frame · cracked.75 INCH CRACK BEYOND STOP DRILL AT MAIN ENTRY DOOR UPPER DOOR UPPER FRAME, AFT END PREVIOUS REPAIR. REMOVED UPPER LINER AND GATE. REMOVED UPPER FRAME. DRILLED REPLACEMENT FRAME. BEGAN INSTALLING FRAME. INST FRAME CLOSED UPPER LINER. PER M/M 52-11-01.SDR DL72S980700Floorbeam · corrosionON UPPER SURFACE OF FLOORBEAM STA 344 FROM LT O/B SEAT TRACK TO DOOR SILL FOUND CORROSION. INSTALLED NEW FLOORBEAM PER SRM 53-10-8 FIG 11.SDR DL72S980727Frame · crackedAT HMV, FOUND FS 930 LT SIDE FRAME IS CRACKED 10 INCH BELOW CABIN WINDOW. FABRICATED NEW PARTS SRM 53-10-4, PAINTED/INSTLD COMPLETED PER SAME.SDR DL72S980660Blkhd Stiffener · crackedCRACKS WERE FOUND IN THE LBL AND RBL 36.83 VERT STIFFENER ON THE FWD SIDE OF THE FS 1183 BLKHD. THE CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIRED PER ERA 331543-14.SDR DL72S980659Fuel Control · failedNR 3 ENG DID NOT RESPOND TO THROTTLE MOVEMENT DURING DESCENT, FLAMEOUT, FUEL FLOW WAS ZERO. EGT AND EPR WERE ZERO AND NOT RESPONDING. N1 AND N2 DISPLAYED WINDMILLING INDICATION, THIS LASTED FOR 2 TO 3 MINUTES. PRIOR TO COMMENCING THE ENG FAILURE FOLLOW UP CSDR DL72S980696Bushing · wornBUSHINGS WORN RT HORZ STAB. NR 1 HINGE ATTACH PT FOR ELEV FITTING BUSHINGS ARE WORN. ALSO, HARDWARE IS WORN AND FITTING LUGS ARE WORN. SPOTFACED .013 ON D/B FACE OF I/B LUG AND .010 ON I/B FACE OF O/B LUG. REMOVED BUSHINGS AND CLEANED LUGS WITHIN LIMITS PESDR DL72S980657Spar · crackedHORIZ STABILIZER RT ELEVATOR REAR SPAR, REPAIR FOR TYPICAL CRACKS. THE RT ELEVATOR REAR SPAR WAS FOUND WITH TWO TYPICAL CRACKS .25 OR SMALLER EXTENDING FROM UNDERNEATH THE 2ND HINGE FITTING FROM THE OUTBD END OF THE SPAR. THE CRACKS WERE STOP DRILLED PER BACSDR DL72L980646Air Distribution · smokeAIR RETURN SMOKE IN AFT CABIN DURNING T/O CREW DUMPED FUEL TO 163,500 NORMAL LANDING AND STOP. RAN PACKS WITH APU AIR ALL PACKS OPERATED NORMAL. FLT CREW TAXI AND AND RAN ENGINES AT RUNUP AREA WITH MECHANIC, CHECKING PACKS WITH ENGINE AIR AT IDLE AND POWER.SDR DL72K980641Strap · crackedA CRACK WAS FOUND IN THE BEAR STRAP AT THE R1 DOOR CUTOUT. THE CRACK WAS LOCATED IN THE FWD, LWR CORNER OF THE CUTOUT AND PROPAGATED FROM THE EDGE OF THE PART DOWNWARD APPROX 1 INCH. REPAIRED PER ERA 331529-14.SDR DL72S980817Skin · cracked.5 INCH CRACK IN FUSELAGE SKIN AT LOWER INBD CORNER L-4 WINDSHIELD, FROM ATTACH SCREW TO CUTOUT-MARKED. REPAIRED PER SRM 53-30-3 AND ER/A 364469-14.SDR CALA9800583Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT FS 1166 RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-30-2.SDR CALA9800582Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT FS 1090, RBL 24. THE CORRODED AREA WAS CUT OUT, TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 8.SDR CALA9800581Bulkhead Web · crackedINSPECTION FOUND TWO 2 CRACKS IN STA 1183 BULKHEAD WEB ON FORWARD SIDE AT WL 188, RBL 32 AND RBL 35.5. THE CRACKS WERE STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 53-00 AND BOEING DRAWING 65C31446.SDR DL72S980686Angle · partANGLE CRACKED STA 303.9 FWD CABIN LBL 28. REPLACED ANGLE PER SRM 51- 00.SDR DL72S980656Bear Strap · crackedFUSELAGE SKIN R1 DOOR SURROUND UPPER HINGE CUTOUT, REPAIR FOR CRACK IN DOOR SURROUND BEAR STRAP. THE INTERNAL R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND CRACKED AT THE UPPER HINGE CUTOUT. THE SKIN WAS TRIMMED AWAY TO ACCESS THE CRACK. THE CSDR DL72K980624Position Ind · failedTRAILING EDGE DEVICES (OUTBOARD) SPLIT BETWEEN 0 DEG AND 2 DEG. ACCOMPLISHED TRAILING EDGE FLAP ABNORMAL CHECKLIST AND DIVERTED TO JFK. REPLACED OUTBOARD FLAP POSITION IND.SDR DL72S980749Angle · crackedDURING SHOP INSPECTION, A DOUBLER ON THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED ANGLE, 32 FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 FIG 802 BY INSTALLING/REPLACING THE REPAIR DOUBLER.SDR DL72S980748Angle · crackedDURING SHOP INSPECTION, THE NR 3 MIDFLAP WAS FOUND WITH A CRACK IN THE AFT LOWER CLOSEOUT ANGLE, 18 FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.SDR DL72S980623Angle · crackedNR 7 SLAT ACT O/B ATTACH ANGLE CRACKED AT UPPER LOBE. REPAIRED PER MM 57-42-0.SDR DL72S980622Web · crackedNR 8 SLAT ACT I/B AND O/B ATTACH ANGLE CRACKED AT WEB. REPAIRED PER MM 57-20-21.SDR DL72S980621Angle · crackedFOUND ON A1 LETTER CK, NR 8 SLAT LOWER ATTACH ANGLE CRACKED AT THE INBD STOP PAD. REPAIRED PER MM 57-54-0.SDR DL72S980620Stiffener · crackedFOUND ON A1 LETTER CK, 1 INCH CRACK IN LOWER END OF L/E SPAR STIFFENER NR 2 SLAT O/B TRACK, INBD STIFFENER. REPAIRED PER MM 57-20-21.SDR DL72S980617Frame · corrodedSKIN ATTACH FLANGE AT FS 1166 FRAME WAS CORRODED BETWEEN S28 AND 29 ON THE LT SIDE. REPAIR WILL REQUIRE REACOMMPLISHMENT OF AD92-12-03. REPAIRED PER ERA 331479-14AD.SDR DL72S980616Bulkhead Ftg · damagedTHE BORE OF FS 870 BLKHD LT TERMINAL FITTING WAS O/S TO 4.605 DIAMETER TO REMOVE TOOLING DAMAGE. REWORKED PER ERA 331517-14.
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