Boeing 737-8
Service difficulty reports · 6,799
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 = '7378' 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 = '7378' 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 SWAA2022012562968Battery Pack · inoperativeFWD GALLEY FLASHLIGHT INOP / [01] R/R BATT. PACK PER AMM 25-64-00; [02] R/R BATT. PACK PER AMM 25-64-00; [03] R/R BATT. PACK PER AMM 25-64-00SDR SWAA2022012563077Slide · detachedFWD SERVICE DOOR SLIDE CAME OFF DOOR ; / [01] RESECURED ESCAPE SLIDE PACK PER AMM 25-66-01 NO DEFECTS NOTED A/C OK FOR SVCSDR SWAA2022012462288Battery · inoperativeAFT GALLEY CAPT SIDE FLASHLIGHT INOP ; AFT GALLEY CAPT SIDE FLASHLIGHT INOP. OK TO CONTINUE PER MEL 25-64-02 SP1B; [02] R&R AFT GALLEY CAPT. SIDE FLASHLIGHT BATTERY PER AMM 25-64-00. OPS CHECK GOOD.SDR SWAA2022012161989Lens · missingEMERGENCY DOOR SIGN COVER MISSING RIGHT SIDE OF AIRCRAFT. INSTALLED SIGN COVER PER AMM 33-51-00SDR 2022F00048Cable · out of adjustCAPTAIN REPORTED THAT DURING FLIGHT, FUSELAGE VIBRATION WHWN THRUST REDUCTION, MAITENANCE PERSONNEL PERFORMED AN AIRFRAME VIBRATION, CONDITIONAL INSPECTION TO AICRAFT, DETECTING THE ELEVATOR CABLES WITH LACK OF ADJUSTMENT, THE RIGGING ON ELEVATOR CABLES WERE PSDR SWAA2022011861437Bulb · inoperativeASD GALLEY EMERGENCY LIGHT HAS INOP BULB ; / [01] REMOVED AND REPLAMPED AFT GALLEY RIGHT SIDE EMERGENCY EXIT SIGN 1 BULB AND PERFORMED GOOD EMERGENCY LIGHT INSTALLATION TEST IAW AMM 33-51-01-960-801 STEP 2.C.(1)(C);(2).; [02] VERIFIED REMOVED AND REPLAMPED AFTSDR SWAA2022011861436Battery Pack · faultedAFT LEFT IB EMERGENCY FLASHLIGHT INDICATOR RED ; / [01] R&R AFT LEFT IB EMERGENCY FLASHLIGHT BATTERY PACK PER AMM 25-64-00. OPS CHECKS GOOD.SDR SWAA2022011360814Lens · missingEMERG. OVERWING EXIT DOOR SIGN @ 14 DEF MISSING LENS COVER ; / [01] REPLACED LENS COVER & OPS NML IAW AMM 33-51-01SDR SWAA2022011460274Door · brokenFUSELAGE DRAIN FWD OF NOSE E BAY DOOR IS BROKEN. REMOVED AND REPLACE FUSELAGE BILGE DRAIN FWD OF NOSE BAY DOOR PER AMM 53-31-03-420; [02] VERIFIED CORRECTIVE ACTION STEP 1.SDR AALA202201119070Latch · lack of lubeAIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR DIFFICULT TO OPEN FROM CABIN WHEN UNLOCKED. LUBRICATED COCKPIT DOOR STRIKER LATCH. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-00-501.SDR SCNA20223025020None · noneDEFECT: EMERGENCY EXIT LIGHTS GUARD OVER SWITCH DAMAGED. RESOLUTION: REMOVED AND REPLACED EMERGENCY EXIT LIGHT SW. GUARD. OPS CHECK NORMALSDR SWAA2022011059301Flashlight · inoperativeAFT LEFT FLIGHT ATTENDANT FLASHLIGHT IS NOT INDICATING. / [01] R+R FLASHLIGHT PER AMM 25-64-00SDR SWAA2022010658953Lamp · inoperativeFOUND EMERGENCY LIGHT BY FWD SERVICE DOOR INOP. RE-LAMPED EMERGENCY LIGHT BY FWD SERVICE DOOR IAW AMM 33-51-04. OPS CHECK GOODSDR SWAA2022010357314Battery · faultedREPORTED BY CREW: FWD R/H FLIGHT ATTENDANT FLASH LIGHT BATTERY LOW LIGHT FLASHING. ; / [01] REMOVED AND REPLACED FWD R/H FLIGHT ATTENDANT FLASH LIGHT BATTERY PER AMM 25-64-00. OPS CHECKS GOOD.SDR 2021FA0000430None · noneAIRCRAFT WOULD NOT PRESSURIZE DUE TO L1 DOOR PRESSURE LEAK. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM PER AMM 52-11-00. OPS CHECK AND PRESSURE CHECK NORMAL. AIRCRAFT OK FOR SERVICESDR ASMF202201250033Engine · malfunctionedLEFT ENGINE NON-SYNCHRONOUS VIBRATIONS ALERT OF REMOTE DIAGNOSTIC GE, DURING TRANSIT CHECK AT MEX AND IN ACCORDANCE WITH CNR 20211223035 OF REMOTE DIAGNOSTIC GE/LEAP SYSTEM, THE LEFT ENGINE HAD MULTIPLE REPORTS FOR ELEVATED LEVELS OF NON-SYNCHRONOUS VIBRATIONSSDR SWAA2021122755933Pcu · failedAIRCRAFT ROLLED RIGHT DURING CLIMB. ; CLIMING THROGH FL220 WITH ATOPILOT ENGAGED IN VNAV SPEED; AIRCRAFT ANKED SLIGHTLY TO THE RIGHT NCOMMANDED AND SPOILERS LIGHT ILLMINATED ON FLIGHT CONTROL PANEL AND REMAINED. / [01] REMOVED AND REPLACED #10 SPOILER PCU CONNSDR SWAA2021122254872Charger · faultedF/O SIDE AFT GALLEY FLASH LIGHT BLINKING RED ; FO SIDE AFT GALLEY FLASH LIGHT LINKING RED / [01] R + R FLASHLIGHT BATTERY REF AMM 25-64-00SDR CALA2021122002405Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRAC KED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00124, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEESDR CALA2021122002404Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00123, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SSDR CALA2021122002403Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00122, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SSDR CALA2021121402361Computer · unserviceableSHORT FINAL TOO LOW GEAR AND PULL UP MSGS. GEAR AND FLAPS WERE P ROPERLY COFIGURED FOR LANDING. CHECKED PIN B9 ON D1153B (GEAR POSITION DISCRETE) WHILE CYCLING PART INFO ENTRY. INSTALLED GPWS COMPUTER AND COULD NOT LOAD SOFTWARE PART IS BAD GEAR HANDLE. NO DEFSDR SCNA20211220102Flap System · faultedFLAP DISAGREE UNCOMMANDED FLAP RETRACTI0ON FROM,30 TO 25 AT 200 ON LANDING PERFORMED FIM TASK 27-51 TASK 830, NO DEFECTS NOTED. R & R FSEU PRECATUINARY REF AMM 27-51-01. OPS CHECKS GOOD FLAP DISAGREE- GO AROUND EXECUTED. LANDED SAFELY IN RFDSDR SCNA20211220101Flap System · unknownFLAP DISAGREE ON APPROACH. SELECTED FLAPS 30 AND FLAPS WERE VERIFIED AT 30. LATER WITHOUT EXCESSIVE SPEED FLAPS WENT TO 25 AND LOCKED OUT. PERFORMED FSEU BITE PROCEDURE. FOUND FAULT TE FLAP UC MSG NO. 27-51351. RESET FAULT AND PERFORMED TE ASSYM SKEW INDICATISDR SWAA2021121452637Fuse · inoperativeEMERGENCY LIGHT OUTSIDE OF FWD ENTRY DOOR INOP ; / [01] RELAMPED. NO FIX. REPLACED A FUSE IN THE BATTERY CHARGER IAW AMM 33-51-06 OPS CHECK GOODSDR ASMF202112080321Access Door · leakingFUEL LEAK AT RIGHT FUEL TANK ACCESS DOOR STEAK NUMBER 7. DURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK AT RIGHT FUEL TANK ACCESS DOOR STEAK NUMBER 7. MAINTENANCE PERSONNEL PERFORMED A RIGHT TANK ACCESS DOOR DAMAGED; SO THE RIGHT FUEL TANK ACCESS DOOR STEAKSDR SCNA20211215100Drain Mast · inoperativeAFTER DESCENDING TO FL 280 FLIGHT ATTENDANTS NOTICED A VIBRATION THAT STARTED A COUPLE OF ROWS AFTER THE EXIT ROW. IT GOT WORSE TOWARDS THE AFT AND WAS WORSE AROUND THE L2 DOOR. IT WAS LOUD AT TIMES AND COULD BE FELT IN THE FLOOR AND SEATS. FA SAYS VERY STRONGSDR SWAA2021120950519Light · inoperativeSIDEWALL LIGHT INOP AT EMERGENCY EXIT SEAT 14F. ; / [01] OK TO CONT. PER MEL# 33-21-01A SP1 AUTH# 37473. R/R EMERGENCY EXIT SIDEWALL LIGHT ASSY. AT 14 DEF IAW AMM 33-21-00. OPS CK GOOD.SDR SCNA20211208099SUWire · chafedVERIFY THE WIRE INTEGRITY AT THE BELOW LISTED CONNECTORS AND MEGGER THE WIRING LOOKING FOR SHORTS. WHILE USING THE MEGGER METER. FOUND 3 TWISTED SHIELDED PAIR WIRES AFFECTED. JUST INBD FROM #4 CANOE ON RT WING. WIRES THAT WHERE CHAFFED WHERE W1032-2006-R2, W1SDR SCNA20211208099Sensor · faultedDEFECT: HAD TRAILING EDGE FLAP DISAGREE ON APPROACH AFTER VECTORS INDICATED 0 WHEN LEVER SAET AT 15 RAN QRH THEN RECEIVED ASYMETRY RAN QRH AND LANDED RESOLUTION: PERFORMED FIM 27-51 TASK 801. FOUND FAULT 27-53280 R28VAC EXC INV. FOUND RT SKEW AND IND BREAKERSDR CALA2021120102227Structure · dentedUPON INSPECTION OF REPAIR IN NOSE AREA STA.200 R/H SIDE JUST UNDER WINDSHIED. A DENT WAS FOUND ABOUT 3" O/B OF CUTOUT(MARKED). REF. LOGPAGE 7514449 & AVO#7251-21-11-28-01. DENT WIDTH IS 0.70", LENGTH 0.50" ,& (DEPTH Y = 0.005") W/Y= 140 VERIFIED DENT MEASUREMESDR CALA2021120102224None · damagedAC 267 RIGHT WINGLET STRUCK UPPER SECTION OF RADOME, DAMAGE RUNS FROM 1OCLOCK TO 3OCLOCK 6 " FROM FUSELAGE PLUS DAMAGED 5 VORTEX GENERATORS ON CAPT SIDE, FO WINDSHIELD WIPER DAMAGED, R1 WINDOW SEAL SMALL DAMAGE TO RUBBER SEAL LOWER LEFT CORNER AND MIDDLE OF SSDR CALA2021120102223Structure · damagedREFERENCE 7504156 COMPLETED DAMAGE CUTOUT ON DENT R/H SIDE ...REF SRM 51-10-02...AWAITING AVO/EC/RA FOR FURTHER INSTRUCTIONS. HFEC INSPECTION REQUIRE AROUND THE CUTOUT. HFEC INSPECTION REQUIRE OF ALL REMOVED INITIAL FASTENERS. PERFORMED HFEC OF TRIM OUT REF 73SDR SWAA2021120148456Lens · looseFWD EXIT SIGN (DOOR 1L) HAS FALLEN OFF. ; / [01] RESECURED EXIT SIGN LENS AT FWD ENTRY DOOR PER SIP.SDR SCNA20211208098Sensor · faultedDEFECT: ON DEPARTURE THE FLAPS WOULD NOT RETRACT, PER QRH ALTERNATE FLAP EXTENSION WAS ATTEMPTED IMEDIATELY A TRAILING EDGE ASSYMETRY DEVELOPED ALT FLAP EXTENSION WAS STOPPED FLIGHT LANDED FLAPS 5 NOTIFIED MC RESOLUTION: PERFORMED FIM 27-59 TASK 807. FOUND #SDR SCNA20211124097Circuit Breaker · trippedON ARRIVAL FLAPS FAILED TO EXTEND. PER THE QRH ALETERNATE FLAP EXTENISON WAS ATTEMPTED. LEADING EDGE DEVICES EXTENTED BUT TRAILING EDGE FLAPS DID NOT. NOTIFIED MC SR 8092. PERFORMED FIM 27-51 TASK 801 FOUND FAULT 27-53280 AND FOUND C/B P6-2 (A11) POPPED RESSDR SWAA2021112446601Retainer · out of adjustFLIGHT ATTENDANT REPORTS THAT THE FORWARD ESCAPE SLIDE GIRT BAR ON THE SERVICE DOOR IS LOOSE. ; / [01] SECURED GIRT BAR TO THE GIRT BAR RETAINER CLIP AND ADJUSTED CLIP TENSION PER AMM 25-66-01.SDR SWAA2021112446594Flashlight · failedAFT LEFT INBOARD EMERGENCY FLASH LIGHT TEST RED ; / [01] R&R AFT LEFT INBOARD FLASHLIGHT PER 25-64-00SDR 2021F00345Unknown · vibrationLEFT ENGINE REACHED 4.1 UNITS OF VIBRATION, CAPTAIN REPORTED THAT DURING CLIMB, THE LEFT ENGINE REACHED 4.1 UNITS OF VIBRATION; SO FLIGHT CREW ACCOMPLISHED THE QRH 7.26 PROCEDURE AND THE VIBRATION WAS STABILIZED IN 3.5 UNITS. MAINTENANCE PERSONNEL PERFORMED A SDR SWAA2021111944104Floor Panel · damagedFLOOR BOARD PANEL NUMBER 241DF POPPING ; FLOOR OARD PANEL NMER 241DF POPPING / [01] RE APPLIED FLOOR PANEL TAPE PER AMM 53-21-00.SDR SWAA2021111743555Girt Bar · disengagedFWD SVC DOOR OPENED WITH GIRT BAR ENGAGED SLIDE DID NOT DEPLOY ; / [01] RE-INSTALLED FWD SVC DOOR SLIDE PER MT 825-PRD-01-01SDR CALA2021111002084None · looseCOACH SEATS 23,25, AND 26C, EPL SHROUDS ARE LOOSE. SECURED ALL EPL SHROUDS LISTED ABOVE IAW CMM 25-21-65, ALL EPL OPS. TEST GOOD.SDR SWAA2021111041941Circuit Breaker · trippedON CLIMB OUT FA CALLED AND SAID ALL GALLEY POWER WAS OUT AT ALL FOUR GALLEY STATIONS. COMPLIED WITH QRH (NOTHING IN THERE); CHECKED CIRCUIT BREAKERS; NONE POPPED. SPOKE TO MX; CONT IN FAULT DESCR ; ON CLIMB OUT FA CALLED AND SAID ALL GALLEY POWER WAS OUT AT ALSDR SWAA2021110539456Battery · inoperativeAFT GALLEY FLASHLIGHT WILL NOT TEST. ( EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ; AFT GALLEY FLASHLIGHT WILL NOT TEST. ( EMERGENCY FLASHLIGHT HOLDERSFLASHLIGHTS ) / [01] REPLACED BATTERIES ( AMM 25-64-00 CL#96827)SDR SWAA2021110439151Battery Pack · inoperativeAFT GALLEY FLASHLIGHT WILL NOT TEST. REPLACED BATTERY PER AMM 25-64-00. OPS CKS NORMAL.SDR SCNA20211101096Connector · dirtyDEFECT: INFLIGHT "ANTISKID INOP" LIGHT ILLUMINATED. RAN QRH PROCEDURE 14-1. RESOLUTION: PERFORMED AACU BITE REF FIM 32-42 TASK 801. FOUND FAULT VLV2, CLEANED CONNECTOR, PERFORMED NEW BITE, NO FAULTS FOUNDSDR SWAA2021110137769Battery Pack · inoperativeEMERGENCY LIGHTS IN THE FWD GALLEY ARE INOP / R&R EMERGENCY BATTERY PACKS AT M1675 AND M02816 IAW AMM 33-51-06; OPS CHECK GOOD. TSR# 2021006826POS M1675 TAG ITG8Q0020ERM P/N OFF D717-01-100 S/N OFF 414494 P/N ON D717-01-100SWA SN ON 39511POS M2816 TAG ITG8Q002SDR ASMF2021120800317Starter · leakingLEFT ENGINE WITH OIL LEAK, DURING TRANSIT CHECK, IT WAS A DETECTED AN OIL LEAK ON LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION AT LEFT ENGINE,NO CONFIRMING OIL LEAK; AS A PRECAUTIONARY ACTION AT MEX, AN ENGINE OIL SYSTEM EXTERNAL, FAN COWL AND THRUSSDR ASMF202112080320Oil System · leakingLEFT ENGINE OIL LEAK. DURING TRANSIT CHECK AND IN FOLLOWING UP OF HIGH OIL CONSUMPTION AT LEFT ENGINE, IT WAS DETECTED AN OIL LEAK. MAINTENANCE PERFORMED A REVISION, DETECTING AN OIL LEAK THROUGH THE OIL INLET COVER; SO THE GASKET SEAL P/N 335-108-001-0, S/S; SDR SWAA2021102633260Hinge · brokenAT PUSH TIME; RAMP REPORTED GROUND AIR SERVICE DOOR HINGE BROKEN AND NOT BE ABLE TO CLOSE / REPLACED DOOR PER AMM 52-49-01.
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