Boeing 727-233
Service difficulty reports · 3,034
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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 = '727233' 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 = '727233' 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 08FDEA01850Angle · corrodedRT Z- ANGLE UNDER AUX TANK HAS SEVERAL LOOSE/MISSING NUT PLATES WITH AREAS OF LIGHT CORROSION ON LOWER SIDE OF PANEL VERIFIED MATERIAL THICKNESS, BLENDED OUT CORROSION, VERIFIED Z ANGLE THICKNESS WAS OUT OF LIMITS AFTER BLEND OUT ORIGINAL THICKNESS WAS .056", SDR 08FDEA01446Hose · leakingENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT COMPLIED WITH QRH. AIRCRAFT INCURRED A MAINTENANCE FLIGHT DIVERSION INTO ATL. FLIGHT CREW ADVISED, THAT, THE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED AT APPROXIMATELY 10,000 FT, DURING CLIMB-OUT WITH AN EPRSDR 2008032701Turbine Blades · failedFLT 433 MIA-BLA - CREW REPORTED, LOSS POWER ON NUMBER NR 3 ENGINE ON TAKEOFF. THE CAPTAIN REJECTED TAKEOFF ROLL AT APPROXIMATELY 10 KNOTS. AIRCRAFT RETURNED BACK TO AMERIJET LINE MAINTENANCE FACILITY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MULTIPLE TURBSDR 08FDEA01095Check Valve · leakingINSTANTANOUS LOSS OF HYD SYS A PRESSURE AND QUANTITY. ALL QRH PROCEDURES COMPLETED. NO RESTORATION. FOUND SYS "A" HYDRAULIC MODULAR PACKAGE WITH BLOWNOUT CHECK VALVE. REMOVAL/INSTALLATION OFF MFG 65-17821-14.SDR 08FDEA01051Actuator · failedRED GEAR DOORS LIGHT AND RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AMBER RIGHT GEAR DOOR LIGHT ON S/O PANEL ALSO ILLUMINATED. REPLACED RT MAIN GEAR ACTUATOR IAW AMM 32-32-002-4, AND RT MAIN GEAR CYCLES UP AND DOWN NORMAL WITH NO LEAKS NOSDR 08FDEA00870Controller · unknownCLIMBING OUT OF LAX, PRESSURE CONTROLLER INDICATED -100 FPM (DESCENT) UNTIL 8000'MSL. F/O COMPLAINED OF PAIN IN EARS/TEETH ALMOST IMMEDIATELY. CAPTS EARS ALSO PAINFUL. AT 8000' CABIN BEGAN TO CLIMB PASSING 12000, F/O STILL UNCOMFORTABLE. DIRECTED S/O TO SWITCSDR 08FDEA00663Hose · chafedIN FLIGHT TOTAL LOSS OF "A" SYSTEM HYDRAULICS. "A" SYSTEM HYD QTY WAS FOUND AT 2 GALLON SYSTEM DID NOT RUN EMPTY. FOUND HYD LINE IN ELEVATOR PCP BROKEN AT CLAMPED AREA. REPLACED LINE REF MM 20-10-012-4. OPERATED HYD SYSTEM. OPERATED AND INSPECTED ALL FLSDR 08FDEA00668Skin · dentedLT WING I/B AFT FLAP DENTED AND DELAMINATED AT WBL 124 CUT OUT DAMAGED AREA ON LT WING I/B AFT FLAP LWR SURFACE WBL 124 AND REMOVED DAMAGED CORE. FABRICATED DOUBLER AND CORE PLUG IAW SRM 57-50-2. BONDED CORE AND DOUBLER, AND PRIMED AND SEALED IAW SRM 51-40-2SDR 08FDEA00661Support Beam · crackedNR 7 SPOILER FITTING TO FALSE SPAR ATTACHMENT REPAIR CRACKED AT WS 198. REMOVED ACTUATOR FITTING SRM 51-30-2. REPAIRED NR 7 SPOILER SUPPORT BEAM (FALSE SPAR) IAW DWG NR 5127-57-038 REV C. REINSTALLED SPOILER ACTUATOR FITTING IAW SRM 51-30-2.SDR 08FDEA00660Support Beam · crackedNR 8 SPOILER FITTING TO FALSE SPAR ATTACHMENT REPAIR CRACKED AT WS 198. REMOVED ACTUATOR FITTING IAW SRM 51-30-2. REPAIRED NR 8 SPOILER SUPPORT BEAM (SPAR) IAW DWG NR SR27-57-038 REV C. REINSTALLED SPOILER ACTUATOR FITTING IAW SRM 51-30-2.SDR 08FDEA00659Seat Track · corrodedMAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION AT STA 950A - 1030, BL 46R. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1. TREATED SDR 08FDEA00524Rib · crackedLT HORIZONTAL STABILIZER MAIN BOX INTERIOR RIB CRACKED AT LIGHTENING HOLE STAB STA 188. CUT OUT DAMAGED AREA IAW SRM 55-10-5 FIG2 NAD 55-10-4 FIG2. FABRICATED REPAIR FOR FWD SPAR WEB IAW SRM 55-10-5 FIG 2 PARTS AND AFFECTED AREAS TREATED AND PRIMED IAW SRMSDR 08FDEA00523Rib · crackedLT HORIZONTAL STABILIZER MAIN BOX INTERIOR RIB CRACKED AT LIGHTENING HOLE STAB STA 69. CUT OUT FWD WEB FOR ACCESS IAW SRM 55-10-3 FIG2. FABRICATED REPAIR DOUBLER FOR INTERNAL RIB IAW SRM 55-10-4 FIG 2 AND 55-10-2 FIG2. FABRICATED REPAIR DOUBLERS IAW SRM 55-10SDR 08FDEA00525Spar · damagedLT WING LEADING EDGE FRONT SPAR FASTENER HOLE HAS NO EDGE DISTANCE AT WS 167, LE STA 90. REPAIRED IAW EA 7-5710-116957.SDR 08FDEA00510Control Valve · failedAT ROTATION NR 2 DUCT ANTI-ICE OVERHEAT LIGHT ILLUMINATED TEMP OFF SCALE HIGH . AN QRH FOR ANTI-ICE DUCT OVERHEAT LIGHT. NR 2 ENGINE COULD NOT BE OPERATED ABOVE 1.25 EPR NR 2 DUCT OVERHEAT LIGHT ON MEL 30-11-A NR 2 ENGINE 13TH STAGE VALVE OPEN GOC ADVISED AIRSDR 08FDEA00471Seat Track · corrodedMAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 950 TO STA 950E, BL 0. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM ER 01-049, SRM 53-10-5 FIG 7A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SSDR 08FDEA00470Seat Track · corrodedMAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 870 TO STA 890, BL 0. REMOVED SEAT TRACK WITH OUT OF LIMIT COROSION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM (ER 01-049) 53-10-5 AND 53-10-2 FIG7. LOCATED AND DRLLED NEW SEAT TRACK IAWSDR 08FDEA00469Seat Track · corrodedMAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 1070 TO STA 1130, BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5, 53-10-2 FIG 7A (ER 01-049) LOCATED AND DRILL NEW SEAT TRACK IAW SRM 51-30-5. TREATED ANDSDR 08FDEA00468Seat Track · corrodedMAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 890 TO STA 950, BL 0. REMOVED AND REPLACED SEAT TRACK IAW SRM ER 01-049 AND SRM 53-10-5 AND 53-10-2 FIG 7ASDR 08FDEA00418Frame · dentedAFT CARGO COMPARTMENT INTERIOR, FRAME SURFACE HAS DENT AT STA 950F, STR 25L. REMOVED PREVIOUS REPAIR ANGLE IAW SRM 51-30-2. FABRICATED NEW REPAIR ANGLE IAW SRM 51-20-151-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED ANGLE. TREATED AND PRIMED PART IAW SRM 51-10-2SDR 08FDEA00417Floorbeam · corrodedMAIN CABIN, FLOORBEAM UPPER SURFACE HAS CORROSION AT STA 846, LBL 48. REMOVED SEAT TRACK AND REMOVED SUPPORT TEE IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW TEE BEAM IAW SRM 53-10-2 FIG7 AND 51-30-5.TREATED AND PRIMED AFFECTED AREA IAW SRM 51-10-2. ISDR 08FDEA00414Skin · dentedAFT FUSELAGE EXTERIOR, NR 3 CARGO DOOR SKIN HAS SEVERAL DENTS AT FWD LWR EDGE BS 1090, S26-27R. EVALUATED DENTS AND FOUND OUT OF LIMITS. CUT OUT DAMAGED SKIN IAW SRM 53-00-03 FIG4. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 52-30-1 FIG 6. TREATED AND PRIMSDR 08FDEA00413Seat Track · corrodedMAIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION IN SEVERAL PLACES FROM STA 360 TO STA 380, LBL 48. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-2 FIG 7 AND 53-10-1 FIG3 SRM PAG23. REMOVED SEAT TRACK SECTION IAW 51-30-2. FABSDR 08FDEA00410Skin · corrodedLT WING TO BODY FUSELAGE SKIN SURFACE SHOWS CORROSION AND GOUGE AT LAP JOINT STA 720E, STR 19L. BURNISHED AFFECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG1,2. REMOVED FAIRING FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE DIM 43/4 X 23/4. FABRICATED DOUBSDR 08FDEA00409Skin · corrodedLWR FUSELAGE EXTERIOR SKIN SURFACE SHOWS CORROSION AT BOTTOM SIDE AT STA. 685, S27-28L. REMOVED INTERCOSTAL IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 3A AND 53-30-3 FIG1. FABRICATED DOUBLER AND FILLER IAW SRM 53-10-3 FIG1 AND 53-10-3 FIG3A. TSDR 08FDEA00389Skin · corrodedRT WING TO BODY FUSELAGE SKIN SURFACE SHOWS CORROSION AND GOUGE AT LAP JOINT, STA 720D, STR 19R. BURNISHED DAMAGED AREA IAW SRM 51-10-1 AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG1,2 AND 53-30-2 FIG2. CUT OUT DAMAGED, FABRICATED REPAIR DOUBLER AND REPAIR FILLSDR 08FDEA00387Skin · crackedLT LWR FUSELAGE EXTERIOR SKIN HAS CRACK AT STA 520, STR 23L. 22.500" FWD FROM STATIC PORT CENTER LINE.SDR 08FDEA00336Floorbeam · damagedMAIN DECK FLOORBEAM, UPPER CHORD FWD FLG, IS MISDRILLED, BS 480, LBL 62, WL 208 ACCOMPLISHED HFEC, NO DEFECTS NOTED. APPLIED SEALANT TO AFFECTED HOLE. REF FED EX EA NR 7-5310-113134. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00333Skin · dentedAFT LOWER EXTERIOR FUSELAGE, SKIN CREASED WITH SMALL GOUGE, STA 1183 5", 2" BELOW STR 20L. REMOVED DAMAGE AREA OF SKIN. HFEC CUTOUT, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND FILLER, ALODINED AND PRIMED AND INSTALLED REPAIR, REF SRM 53-30-3 FIG 28 REFSDR 08FDEA00330Channel · crackedMAIN CARGO DOOR SILL, HAT CHANNEL, ATTACHED TO FLOORBEAM HAS A CRACK AT FASTENER HOLE AS MARKED, LOCATED AT STA 540 8", LBL 61", WL 208". REPLACED DAMAGED HAT CHANNEL AT MAIN CARGO DOOR SILL ATTACHED TO FLOORBEAM STA 4404 TO 560 LBL61. MATERIAL IS BAC1517 SDR 08FDEA00322Power Unit · malfunctionedSHORTLY AFTER TAKEOFF LIGHT IN APU FIRE HANDLE FLICKERED FOR SEVERAL MINUTES, FOLLOWED BY A STEADY LIGHT. NO OTHER FIRE INDICATIONS WERE NOTED. APU FIRE HANDLE PULLED, BOTTLE BLOWN. REMOVED AND REPLACED OPERATING POWER UNIT FOR APU FIRE DETECTION IAW B727-2SDR 08FDEA00279Floorbeam · corrodedCORROSION ON LOWER AFT SIDE OF FLOORBEAM TO CAP AT FLOORBOARD ATTACH FWD HOLE AT FS 720D, LBL 48, WL 208. REMOVED CORROSION AND FLOORBEAM WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED. REMOVED UPPER "T" CHORD CAP FROM LBL 10 - LBL 68SDR 08FDEA00277Skin · crackedCRACK IN UPPER RIGHT WING OUTBD PANEL AT WBL 602.5, OF OUTBD AILERON REPAIRED UPPER WING OUTBD. PANEL AT WBL 602.5 REF EA NR 7-5720-113964. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00257Angle · corrodedCORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL FRAME AT STA 1166 AROUND CAMLOC RECEPTACLE HOLES FRONT AND BACK SIDE. LOWER AFT CARGO COMPARTMENT REMOVED BULKHEAD SUPPORT ANGLE, IN REF TO SRM 51-30-2. VERIFIED MAT'L ID AS BAC 1506-1707 7075-T6, A 848SDR 08FDEA00241Rib · crackedLT WING, FWD SPAR, STA 467, LE RIB, UPPER RADIUS CRACKED. REMOVED BLEED AIR DUCT TO GAIN ACCESS. REMOVE WEB AT STA 467 ON FWD SPAR. FABRICATED WEB REF BAC DWG 65-17218, HEAT TREATED ON FORM 8130-1 NR 2008-01-075, TREATED AND PRIMED AND INSTALLED. REF SRM 5SDR 08FDEA00240Bracket · crackedRT WING O/B MOST UPPER TRAILING EDGE PANEL I/B SIDE SPOILER SEAL BRACKET CRACKED AT AFT EDGE AND AT SPOILER DOWN STOP PAD CUTOUT. REMOVED CRACKED BRACKET AND FABRICATED NEW SEAL DEPRESSOR BRACKET REF BOEING DRAWING 65-21657/ITEM NR 155 AND INSTALLED ON PANEL SDR 08FDEA00239Frame · corrodedLWR FWD CARGO PIT FRAME UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE STA. 720D ABOVE STR 26R. FOUND FRAME TO BE OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED FRAME. REINSTALLED Z-ANGLE, VERTICAL BULKHEAD SUPPORT IAW SRM 51-30-2 PG 1-16 SRM 51-40-2 PG 1-6, DSDR 08FDEA00238Frame · corrodedLWR FWD CARGO PIT FRAME, UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE OF STA 720D ABOVE STR 26L. FRAME DAMAGE FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. REMOVED AND REINSTALLED Z-ANGLE, BULKHEAD SUPPORT AND INTERCOSTAL TO SDR 08FDEA00236Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER "T" CAP CORRODED, BS 950D, RBL 9-23 THIS SDR WAS ENTERED IN ERROR AND WILL NOT BE USED. THIS IS A DUPLICATE OF SDR NR 08-0235. THIS SDR ENTERED IN ERROR - ADMINISTRATOR.SDR 08FDEA00235Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, RBL 9-23. REMOVED CORROSION. OUT OF LIMITS IAW SM 53-10-8, SRM 51-10-6. DISPLACED SEAT TRACK BS 950-950F RBL 25 IAW SRM 51-30- 2. REMOVED CHANNEL STIFFNER BS 950D, RBL 25. REMOVED CHANNEL SUPPORT BS 950DSDR 08FDEA00234Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, LBL 10-13. REMOVED CORROSION. FOUND OUT OF LIMITS IAW PF SRM 53-10-1 FIG 4C. REPAIRED DAMAGED FLOORBEAM IAW SRM 53-10-8 PG 18 FIG 3 UPPER CHORD REPAIR. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA00233Seat Track · corrodedSEAT TRACK CORRODED, STA 880-950, RBL 47 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK, ALODINED AND PRIMED AND INSTALLED AT STA 870-950. REF BAC DWG 65-19601, SRM 51-10-2, SRM 51-30-2. REMOVED FUEL SHROUD IN W/SDR 08FDEA00221Intercostal · crackedLEFT LOWER FUSELAGE "B" SYSTEM HYD COMPARTMENT HYDRAULIC LINE SUPPORT INTERCOSTAL CRACKED 3 AREAS IN RADIUS, STA 950A PLUS 4, TO 950A PLUS 7 JUST O/B OF RESERVOIR REMOVED CRACKED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, P/N 69-14299-1. TREATED AND PRIMED, ASDR 08FDEA00220Rib · crackedNR 2 FLAP TRACK MID FRG AFT RIB IS CRACKED REMOVED CRACKED RIB REF SRM 51-30-2 P1, PRIMED AND PAINT FLAP TRACK FRG, REF 51-10-2 PG 1-4. INSTALLED REPLACEMENT RIB REF SRM 51-30-2 P 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00219Frame · corrodedCORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL UPPER FRAME AT STA 1166, AROUND CAM LOC RECEPTACLE HOLES FRONT AND BACK FABRICATED UPPER FRAME AT STA 1166 WL 200, AFT CARGO COMP BULKHEAD, REF SRM 51-30-2 PG 4. REF BOEING DWG 65-67250-5 SHEET 1-5. THSDR 08FDEA00218Stringer Clip · tornCABIN BS 660, S 5L STRINGER CLIP TORN. REMOVED STRINGER CLIP, TRANSFERRED HOLD TO NEW CLIP. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA00217Floor Support · crackedAFT CARGO PIT CAP STRIP, 950D TO 990 LT, CRACKED AT FASTENER HOLE FABRICATED NEW CAP STRIP. REF BOEING DWG NR 65-67278/SRM 51-20-1 FIG 2/SRM 51-10-1, PG 12. TREATED AND PRIMED CAP STRIP, REF SRM 51-10-2 PG 1, THIS IS CLASSIFIED AS MINOR REPAIR.SDR 08FDEA00216Intercostal · corrodedMAIN CARGO DECK INTERCOSTAL CORRODED, BS 1030-1050, LBL 19 REMOVED CORROSION AND FOUND OUT OF LIMITS. MATERIAL THICKNESS IS .071". REMAINING MATERIAL IS .051", AND MATERIAL LOSS AT .019'' REF SRM 53-10-1. BACKED DRILLED NEW INTERCOSTAL AT BS 1030-1050, LSDR 08FDEA00212Bracket · crackedRT WING, NR 6 FLAP TRACK FAIRING, O/B SKATE ANGLE ATTACH BRACKET, CRACKED AT I/B AFT SIDE REMOVED RT WING NR 6, FLAP TRACK FAIRING O/B SKATE ANGLE ATTACH BRACKET I/B AFT SIDE IAW SRM 51-30-2 PG3, VERIFIED MATERIAL AS MATERIAL 2024-T3 .071" IAW DWG 65-28115-5 SSDR 08FDEA00211Link · corrodedMAIN DECK 1L DR CUTOUT LWR HINGE RADIUS LINK IS CORRODED. INSTALLED NEW RADIUS LINK, REF MM 52-11-001-PG 2, OPS CHECKED GOOD THIS IS CLASSIFIED AS A MINOR REPAIR.
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