Boeing 727-232
Service difficulty reports · 6,539
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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 = '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 DL72S954012Bushings · looseATL - HMV, NR 5 FLAP TRACK, FWD HINGE FITTING FOR MLG STRUT DOOR HAS LOOSE BUSHINGS. REMOVED BUSHINGS, REAMED BORE TO .750, ACCOMPLISHED BUSHING REPLACEMENT PER MM 57-43-0.SDR DL72S954011Bushings · looseATL - HMV, NR 4 FLAP TRACK FWD HINGE FITTING FOR MLG STRUT DOOR HAS LOOSE BUSHINGS. REMOVED BUSHINGS, REAMED BORE TO .750, ACCOMPLISHED BUSHING REPLACEMENT PER MM 57-43-0.SDR DL72S953859Angle · crackedDURING F-1 LETTER CHECK, FOUND NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S953858Angle · crackedDURING F-1 LETTER CHECK, FOUND NR 7 L/E SLAT COVE SKIN ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72L953930Stringer · damagedDURING CV-2 CHECK, STA 990 FRAME WAS CUT TO FACILITATE MTC OF STRINGER 29L REF NR 95. REPAIRED PER M/M 53-12-0 PG 806 AND 807 FIG 805.SDR DL72S954035Skin · damagedWING SKIN, CENTER TANK UPPER SKIN STA 761 LBL 65, TWO EXISTING FASTENER HOLES IN THE WING CENTER SECTION UPPER PANEL WERE DAMAGED ON THE UNDERSIDE REQUIRING OVERSIZING. THE TWO HOLES ARE LOCATED AT FS 761 AT APPROX LBL 65. THE REPAIR OVERSIZES BOTH HOLES IN SDR DL72S953847Le Skin · wornDURING SHOP INSPECTION, NR 1 MIDFLAP L/E SKIN WAS FOUND WITH WEAR DAMAGE AT THE O/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 803.SDR DL72S953836Web · crackedDURING B-1 LTR CHECK, FOUND 48 SEC TORQUE BOX WEB IS CRACKED AT LIGHTENING HOLE, STA 1323 LT. REPAIRED PER MM 53-11-0.SDR DL72L953875Web · crackedDURING CV2 CHECK, FOUND .25 INCH CRACK AT LIGHTNING HOLE, INBD VERT WEB RT STA 1225. REPAIRED PER M/M 53-11-0.SDR 95FDEA01433Skin · corrosionCORROSION FWD BAY, ON AND UNDER BONDED DOUBLER AT BL 0, BS 720-726 AT VARIOUS BODY STAT, IT IS DISBONDED, ALSO, (ACCESS IS REQUIRED). REMOVED AND REPLACED BELLY SKIN FROM BS 680-740, STR 26 LT AND RT ALL WORK DOWN IAW FEDEX EA 7-5300-25764 AND DRAWING NR 65-5SDR 95FDEA01429Skin · dentedEA 7-5330-25397 CORRECTIONS FOR DENT IN FUSELAGE SKIN/CARGO DOOR DOUBLER (LOGBOOK ENTRY REQUIRED) MACH NR 53-30/686. REMOVED DAMAGED STR 24L, RECONTOURED DENT, INSPECTED FOR CRACKS NONE FOUND. FABRICATED STR AND DOUBLER REPAIR AND INSTALLED REPAIR PARTS AT BSDR DL72S953941Le Skin · wornDURING SHOP INSP, NR 3 MIDFLAP WAS FOUND WITH I/B L/E SKIN WORN. REPAIRED LEADING EDGE PER MM 57520, BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER.SDR DL72S953877Shim · misalignmentDURING ROUTINE INSECTION, THE LAMINATED SHIM INSTALLED ON THE RIGHT WING I/B FLAP TRACK WAS FOUND TO HAVE MIGRATED FROM LEFT TO RIGHT. COMPLYING WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED, REINSTALLED AND THE ATTACHMENTS WILL BE RETORQUED. INSPECTSDR DL72S953828Doubler · crackedFOUND DURING C-1 LETTER CHECK - DOUBLER UNDERNEATH I/B STOP PAD NR 7 SLAT IS CRACKED. REPAIRED PER MM 57-54-0 PAR 12.SDR DL72S953827Skin · crackedFOUND DURING C-1 LETTER CHECK - .75 INCH HOLE IN 48 SEC TORQUE BOX SKIN RT STA 1308 - .3750 INCH CRACK IN 48 SEC TORQUE BOX SKIN AT LIGHTNING HOLE STA 1235 RT. REPAIRS MADE PER M/M 53-11-0, PGS 802 - 832, AND 833.SDR DL72S953826Rib · crackedFOUND DURING C-1 LETTER CHECK - 1.25 INCH CRACK IN RIB ON NR 7 SLAT I/B OF I/B TRACK. REPAIRED PER MM 57-54-0.SDR DL72S953819Spar · crackedDURING INSPECTION, RT WING AILERON WAS FOUND WITH REAR SPAR CRACKED. REPAIRED PER SRM 51-40-3.SDR DL72S954034Skin · crackedFUSELAGE SKIN REPAIR AT AFT LAVATORY SERVICE PANEL CUTOUT, FS 1158 TO FS 1183, BETWEEN STRINGERS 20L AND 24L. DURING THE ACCOMPLISHMENT OF EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND CRACKED AND CORRODED IN THE UPPER FWD CORNER OF THE AFT LAVATORY SSDR DL72S953949Skin · corrodedHEAVY CORROSION WAS FOUND JUST FORWARD OF STA 720 AND OUTBOARD OF STR 28R AND, ALSO, AFT OF STA 710 AND OUTBOARD OF STR 27L. THERE ARE THREE EXISTING DOUBLERS IN THIS REPAIR AREA. THIS ER/A WILL REMOVE THE DAMAGED SECTION OF SKIN AND REPAIR THE DAMAGE WITH ASDR DL72S953942Skin · wornDURING SHOP INSP, NR 4 MIDFLAP L/E SKIN WORN AT O/B END OF FLAP. REPAIRED PER MM 57520 BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER.SDR DL72S953920Angle · crackedTHE NR 5 L/E SLAT, LOWER T/E ATTACH ANGLE CRACKED AT RIB NR 9. REPAIRED PER M/M 57-54-0 PAGE 807A.SDR DL72S953903Spar · crackedAFT SPAR CHORD WAS FOUND CRACKED 33, 54 AND 61 FROM IB END OF NR 3 MIDFLAP. THE DAMAGED SECTION WAS REPLACED AND SPLICED IN PER MM 57-50-00.SDR DL72S953818Cowling · crackedDURING A SHOP INSPECTION, THE UPPER FRAME ANGLE WAS FOUND TO BE CRACKED. A REPAIR WAS INSTALLED PER THE S.R.M. 54-10-3. FOR NR 2 ENGINE LEFT FORWARD COWL PANEL.SDR 95FDEA01468Gusset · corrosionCORROSION FWD BAY ON PRESS GUSSET AT BS 740 AT KEEL BEAM, STR 28R WL 145. REMOVED CORROSION FROM PRESS GUSSET AT BS 740 STR 28R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED GUSSET AND INSTALLED NEW GUSSET, BS 740 STR 28R. FUNCTIONAL CHECK PER MM FSDR 95FDEA01467Fail-Safe Chord · corrodedCORROSION FWD BAY ON TOP SIDE OF BS 740 FAIL-SAFE CHORD LBL 9 TO LBL 14. ALSO, 4 FASTENERS UNDERSIDE, 2 AT STR 27L AND 2 AT STR 27R, ACCESS IS REQUIRED. REMOVED CORROSION ON FAIL-SAFE CHORD BS 740 FROM LBL 18 RBL 16, FOUND CORROSION TO BE OUT OF LIMITS PER FSDR DL72S953811Eel Battery Pack · dischargedDURING EMERGENCY LIGHTS TEST, FOUND EXIT LIGHTS ABOVE BOTH WING EMERGENCY EXITS WERE INOP. REPLACED BATTERY PACK M1086 AND LIGHTS NOW TEST GOOD.SDR DL72S953808Acl Wire · shortedON CLIMB-OUT, UPPER FUSELAGE ANTI-COLLISION LIGHT FELL OUT OF MOUNT AND CAUSED POWER WIRES TO SHORT, WITH RESULTING SPARKS AND SMOKE IN CABIN. FLT RETURNED TO CAE. FOUND DAMAGED WIRES ON LIGHT ASSEMBLY. REMOVED ASSEMBLY, SECURED WIRES, PLACED ON MCO. LIGHTSDR CAL950855Actuator · leakingFLT NR 0209 - CUN - THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE FROM IAH TO SAL. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO CUN. WHILE ON APPROACH TO CUN, THE NR 6 SLAT WOULD NOT COME DOWN AND LOCK USING THE ALTERNATE FLAPSDR DL72S953846Eel · inoperativeAFT AIRSTAIR EMERGENCY EXIT LIGHTS ARE INOP. REPLACED LIGHT ASSEMBLY AND BATTERY PACK OPERATION NORMAL.SDR DL72S954010Rib · crackedATL - HMV, RIB CRACKED NR 7 LE SLAT NR 10 RIB CRACKED ON TOP FLANGE. ROUTED OUT DAMAGE AND FABRICATED DOUBLER PER MM 57-54-0 PG 819. FABRICATED FILLER, INSTALLED DOUBLER AND FILLER PER M/M 57-54-0 PG 819.SDR DL72S953879Frame · misdrilledDURING THE ACCOMPLISHMENT OF DAL EO 4-58560-3AD, IT WAS NOTICED BY MAINTENANCE THAT THE FRAME REINFORCEMENT STRAP ON THE OUTER CHORD OF STA 760.95 FRAM, WAS DOUBLE DRILLED AT THREE LOCATIONS PRIOR TO THIS HEAVY MAINTENANCE VISIT. MAINTENANCE OVERSIZED THE HOLSDR DL72S953800Angle · crackedFOUND ON A2 LETTER CHECK, NUMBER 7 SLAT COVE SKIN ANGLE CRACKED .25 INCH IN UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.SDR DL72S953799Angle · crackedFOUND ON A2 LETTER CHECK, NR 1 SLAT COVE SKIN ANGLE CRACKED AT THE OUTBOARD STOP PAD. REPAIRED PER MM 57-54-0.SDR DL72L954033Skin · corrodedFUSELAGE SKIN, FS 720 TO 720B S-26R BL 0, CORROSION REPAIR. CORROSION ON THE LOWER SKIN PANEL REQUIRED CUT OUTS IN FOUR AREAS LOCATED FROM FS 720 + 10 TO 720B BETWEEN STRINGERS 26R AND BL 0. TWO OF THE CUT OUTS ARE UNDER THE LAPPED SKIN AT STRINGER 26R. THESDR DL72S954009Angle · crackedATL - HMV, ANGLE CRACKED NR 2 K-FLAP ACT MOUNT, INBD LOWER ANGLE IS CRACKED. REMOVED ANGLE, STOP DRILLED CRACK, DRILLED REPAIR DOUBLER PER MM 57-20-21 PG 811 AND INSTALLED REPAIR DOUBLER PER MM 57-20-21.SDR DL72S953958Trunnion Ftg · corrodedUPON HMV, FOUND LT MLG FWD TRUNNION FITTING INNER FACES CORRODED. REMOVED BUSHINGS...BLENDED SURFACES WITHIN LIMITS PER M/M 57-43-0.SDR DL72S953874Fitting · corrodedRT MLG FWD TRUNNION FITTING INSIDE FACES CORRODED. ALSO, EVIDENCE OF CORROSION UNDER BUSHINGS. REMOVED BUSHINGS AND CORROSION, BORED HOLES, SPOTFACED HOLES WITHIN MM 57-43-0 LIMITS. MACHINED LOWER O/B BUSHINGS PER DRAWING NR 69-49502-7 AND MM 57-43-0 PG 403SDR DL72S953873Trunnion · corrodedNOSE GEAR RT TRUNNION BORE CORRODED. CLEANED ATTACH BOLT HOLES, MACHINED BORE TO 2.525 TO REMOVE CORROSION. ROTOPEENED, TREATED, PRIMED, MFG BUSHINGS AND INSTALLED BUSHINGS PER MM 53-40-0.SDR DL72S953803Angle · crackedANGLE CRACKED, WING TRAILING EDGE BELOW NR 8 SPOILER ATTACH BRACKET FOR ACTUATOR. STOP DRILLED CRACK, INSTALLED REPAIR PER M/M 57-20-22 PG 809.SDR DL72S953791Eel Battery Pack · dischargedDURING LAYOVER, EMERGENCY LIGHT AT C-2 CARGO DOOR INOP. REPLACED BATTERY PACK M957, OPERATION NORMAL.SDR 95FDEA01400Splice · corrodedCORROSION (71C209-02), ON STR SPLICE BS 680 STR 27R WL 148. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR SPLICE AT BS 680 STR 27R WL 148 IAW SRM 53-10-1.SDR DL72S954036Skin · corrodedBELLY SKIN, CORROSION AT STA 700 TO 720, O/B OF S-28L AD 91-09-09, 94-05-04. SKIN CORROSION AT STA 700 TO 720, O/B OF S-28L HAS PROMPTED REQUEST FOR AN EXTENSION OF AN EXISTING DOUBLER IN THAT AREA TO COVER THE ADDED DAMAGE REMOVAL, APPROXIMATLY 2 BY 2 INCHESSDR DL72S953872Attach Mount · corrodedNOSE LANDING GEAR LEFT ATTACH MOUNT CORRODED. CLEANED BOLT HOLES, MACHINED BORE TO 2.617, REMOVED CORROSION AND ROTOPEENED. TREATED, MANUFACTURED BUSHINGS, CAD BUSHING AND INSTALLED BUSHINGS PER MM 53-40-0.SDR DL72S953779Rib · crackedDURING HMV, FOUND ON VERTICAL FIN 4TH RIB DOWN FROM ACCESS HOLE STA 6.372 RIB NR 6 CHORD ANGLE CRACKED AT STR 7 LEFT. REPAIRED PER M/M 55-30-0 PG 802.SDR DL72S953778Rib · crackedDURING HMV, FOUND NR 8 SLAT, RIB NR 13 WAS CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S953752Eel · inoperativeEXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOP. NEEDS RACK M957 FWD TO MCO AND PLAC. REPLACED RACK, OPERATION NORMAL.SDR DL72S953751Eel · inoperativeCOCKPIT EMERGENCY LIGHT INOP. REPLACED RACK, OPS NORMAL.SDR DL72S953777Rib · crackedDURING HMV, FOUND NR 4 SLAT HAS CRACK AT ACTUATOR ATTACH O/B RIB. REPAIRED PER MM 57-54-0 FIG 804.SDR DL72S953776Rib · crackedDURING HMV, FOUND NR 3 SLAT HAS CRACK IN LOWER SURFACE OF NR 3 RIB FROM I/B END. REPAIRED PER MM 57-54-0 FIG 805.SDR DL72S953748Angle · crackedFOUND DURING HMV - NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED PER M/M 57-54-0, FIG 812.
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