Boeing 737-8Q8
Service difficulty reports · 1,686
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 = '7378Q8' 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 = '7378Q8' 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 SCNA20220915105S1None · noneSUPPLEMENTAL: DEFECT 920979: N/R-00002: TRANSFERED FROM DEFECT #720979 ITEM #1 ON APPROACH, EXPERIENCED A TRAILING EDGE FLAP ASSYMETRY. RAN QRH WHEN SELECTED TO 15 THE FLAPS STOPPED AT 13 PER QRH SELECTED BACK TO 10 FLAPS RETURNED TO 10 AFTER LANDING. NON-ROUSDR SCNA20220915105SUNone · noneSUPPLEMENTAL SCNA20220915105: DEFECT 720979: ON APPROACH, EXPERIENCED A TRAILING EDGE FLAP ASSYMETRY. RAN QRH. WHEN SELECTED TO 15, THE FLAPS STOPPED AT 13. PER QRH, SELECTED BACK TO 10, FLAPS RETURNED TO 10 AFTER LANDING. RESOLUTION: N/R-00007 - DURING TROUSDR SCNA20220915105None · nonePLEASE SEE PREVIOUS SDR SCNA20220815105 SHOULD BE CORRECTION: SCNA20220915105 (UNIQUE CONTROL CREATED IN SEPTEMBER NOT AUGUST)SDR SCNA20220915104None · noneDEFECT 720976: TRAILING EDGE FLAP DISAGREE, FLAP LEVER AT 5 INDICATION FLAPS STOPPED AT 2 DEGREES, MANUAL EXT PER QRH LANDED FLAPS 15. RESOLUTION: INSPECTED SKEW SENSOR CONNECTORS AND FOUND #3 SENSOR C/P LOOSE. SECURED C/P PER AMM 27-59-01 FUNCTIONAL TEST SDR SCNA20220913103None · noneDEFECT 720975 DURING DECENT TO LAND WE GOT A FLAP DISAGREE WHILOE EXTENDING FLAP LEVER TO 5 INDICATION SHOWED RIGHT FLAP STILL AT 2 DEGREES AND LEFT FLAP AT SLIGHTLY LESS THAN 5 DEGREES RAN QRH AND LANDED FLAPS 15. RESOLUTION: PERFORMED FSEU BITE. FOSDR SCNA20220815105None · noneDEFECT 720979: ON APPROACH, EXPERIENCED A TRAILING EDGE FLAP ASSYMETRY. RAN QRH. WHEN SELECTED TO 15, THE FLAPS STOPPED AT 13. PER QRH, SELECTED BACK TO 10, FLAPS RETURNED TO 10 AFTER LANDING. RESOLUTION: (WORK IN PROGRESS)SDR SCNA20220815095SULight · inoperativeSUPPLEMENTAL. DEFECT: 720507: FWD ENTRY LIGHT INOP. RESOUTION: RELAMPED FWD ENTRY LIGHT REF AMM 33-29-00 OPS GOOD. THIS CLEARS MEL MC NOTIFIED.SDR SCNA20220815095Light · inoperativeDEFECT 720502: FWD ENTRY LIGHT INOPSDR SCNA20220808093Flap System · splitCORRECTION: SCNA20220808093 - CORRECT DATE 8/06/2022: DEFECT LOG 699780: SPLIT FLAP IN FLIGHT WHEN GOING UP TO 5. RESOLUTION: R&R #1 FLAP SKEW SENSOR CONNECTOR PER SWPM 20-60-00. R&R LH FLAP POSTION TRANSMITTER CONNECTOR PER SWPM 20-60-00. R&R LH FLAP POSTSDR SCNA20220807093Flap System · splitDEFECT LOG 699780: SPLIT FLAP IN FLIGHT WHEN GOING UP TO 5. RESOLUTION: R&R #1 FLAP SKEW SENSOR CONNECTOR PER SWPM 20-60-00. R&R LH FLAP POSTION TRANSMITTER CONNECTOR PER SWPM 20-60-00. R&R LH FLAP POSTION TRANSMITTER PER AMM 27-58-01. OPS CHECK FAILED. REISDR SCNA20220805090SUFlap System · draggingDEFECT: ON APPROACH THERE WAS FLAP DISAGREE CONDITION: FLAP LEVER WAS SET TO 15 FLAP INDICATION WAS BETWEEN 2 AND 5. CREW ACCOMPLISHED NNC "TRAILING EDGE FLAP DISAGREE" AND FLAPS 15 LANDING. FLAPS LEFT IN 15 AFTER LANDINGRESOLUTION: PERFORMED FSEU BITE PER 27SDR SCNA20220805090Flap System · splitDEFECT: ON APPROACH THERE WAS FLAP DISAGREE CONDITION: FLAP LEVER WAS SET TO 15 FLAP INDICATION WAS BETWEEN 2 AND 5. CREW ACCOMPLISHED NNC "TRAILING EDGE FLAP DISAGREE" AND FLAPS 15 LANDING. FLAPS LEFT IN 15 AFTER LANDING
RESOLUTION: PERFORMED FSEU BITE PSDR SCNA20220805089Flap System · jammedDEFECT: FLAP DISAGREE ON DECSENT EXTENDED NORMALLY TO 15 ON ALTERNATE FLAPS EXTENSION. RESOLUTION: 7/28 - R/R FLAP POSITION TRANSMITTERS, R/R T525 FLAP SKEW SENSOR, ADJUSTED SKEW CONTROL, RIGGED LH FLAP POSITION TRANSMITTER, R/R RH FLAP POSITION TRANSMITTERSDR 2022F00296None · noneBOTH BLEED TRIP OFF ILLUMINATED CABIN WAS UNCONTROLABLE EMERGENCY DESCENT WAS PERFORMED. CORRECTIVE ACTION HAS BEEN DONE BLEED TRIP OFF LIGHTS RESET IAW FIM 36-10 TASK 801 AND DCPC BITE PROCEDURE IAW FIM 21-31 TASK 801 NORMAL OPERATION ON GROUNDSDR SCNA20220622073Lens · damagedDEFECT 690301: L1 DOOR EMERGENCY EXIT LIGHT LENS DAMAGED. RESOLUTION: REPLACED L1 DOOR EMERGENCY EXIT LIGHT LENS AS NEEDED. CHECKS GOOD REF AMM 33-51-01.SDR SCNA22020617070Door Knob · out of adjustDEFECT: FLIGHT DECK DOOR KNOB WILL NOT ROTATE TO UNLOCK POSITION. RESOLUTION: PERFOMRED OPS CK OF FLT DECK DOOR CONTROL SWITCH REF AMM 52-51-00. OPS CK GOOD. THIS CLEARS MEL 52-17SDR SCNA22020617069Control Switch · out of adjustDEFECT: FLIGHT DECK DOOR KNOB WILL NOT ROTATE TO UNLOCK POSITION. RESOLUTION: PERFOMRED OPS CK OF FLT DECK DOOR CONTROL SWITCH REF AMM 52-51-00. OPS CK GOOD. THIS CLEARS MEL 52-17 MDDR #112672SDR 2022F00260None · noneCRACKS WERE FOUND ON HORIZONTAL STABILIZAR LOWE SKIN STA. 129.50 (REF: TASK CARD 55-800-00-01).SDR SCNA20220427033None · noneLEFT SCREDW ON L1 RAFT COMPARTMENT MISSING. RESOLUTION: REMOVED & REPLACED L1 SLIDE SUPPORT FITTING HARDWARE PER CMM 52-16-12. REINSTALLED L1 SLIDE PER AMM 25-16-01 RII A&P 3657911SDR SCNA20220427036Slide & Sleeve · jammed1R DOOR GIRT BAR HOLDER IS LOOSE . GIRT BAR NOT SECURED IN HOLDER. RESOLUTION: ADJUSTED 1R DOOR GRIT BAR HOLDER REF AMM 25-66-00SDR 2022F00126None · noneAUTO FAIL LIGHT ILLUMINATED WITH CABIN ALTITUDE UNCONTROLABLE ALTN LIGHT NOT ON. (FRM 21302000). CORRECTIVE ACTION: HAS BEEN REPLACED CONTROL PANEL PRESURIZATION AND REPLACED PRESSURE CONTROLLER. NOT FOUND FAIL.SDR SCNA20220427037Door · inoperative2L DOOR SLIDE WAS FOUND UNMOUNTED. RESOLUTION: REINSTALLED 2L SLIDE DOOR PER AMM 25-66-01 OPS CHECK GOOD OK FOR SERVICESDR SCNA20220427040Girt Bar · looseL2 GIRT BAR HOLDER LOOSE. RESOLUTION: ADJUSTED HOLDER REF AMM 25-66-00SDR SCNA20220427041Girt Bar · looseL1 GIRT BAR WILL NOT STAY IN CLIPS WHEN OPENING DOOR. RESOLUTION: ADJUSTED CLIPS REF AMM 25-66-01 OK FOR SERVICESDR SCNA20220427042None · noneESCAPE SLIDE ON DOOR 1L IS LOOSE. RESOLUTION: SECURED MATERIAL ON GIRT BAR AND INSTALLED REF AMM 25-66-01-000-804SDR SCNA202217003None · noneDEFECT SECTION 43 FUSELAGE SKIN GOUGED FROM BS414 TO BS438 AT S-20R. RESOLUTION: DAMAGE WAS TRIMMED OUT FROM BS414 TO BS438 AT STRINGER 20R. STRINGER 20R WAS FOUND CRAKCED ATHE THE AFT THREE FASTENER HOLES WHICH WAS TRIMMED AND REPAIRED. A REPLACEMENT STRINGSDR SCNA20220217002None · noneWO 67327: REPAIR OF GROUND DAMAGE TO THE FUSELAGE AT BS 410-440 AND STRINGER 19R-21R. BOEING WAS CONTACTED FOR REPAIR OF THE DAMAGE. RESOLUTION: COMPLIED WITH ACCOMPLISHMENT OF REPAIR PER ATS ER 22-01166 REV IR.SDR SCNA20220217001None · noneTASK: TEMPORARY SKIN REPAIR INSTALLED STA 420 STR 20R. RESOLUTION: REMOVED TEMPORARY SKIN REPAIR AT BS 420 STR 20 AND INSTALLED 1 DOUBLER 2024-T3 .063", -2 TRIPLER 2020-T3 .063" AND -3 FILLER 2024-T3 .090" IAW SUN COUNTRY ENGINEERING TASK CARD ENG-53SCA-1091SDR 2022F00043Control Module · faultedREJECTED TAKEOFF DUE TO MASTER CAUTION OVHT/DET (FAUL APU DET INOP). HAS BEEN DONDE FM 26-10 FIRE DETECTION CONTROL MODULE BITE PROCEDURE IN GRPUND NO FOUND DISCREPANCIES.SDR 2022F00022Fseu · failedL.E. FLAPS TRANSIT DISAGREE WITH FLAPS ASSYMETRY. CORRECTIVA ACTION: REMOVED AND REPLACED FSEU IAW AMM 27-51-01/401. BITE TEST IAW AMM 27-51-00-740-8001 TEST NORMAL.
(AIRCRAFT EXPORTED, REGISTRATION NUMBER AS OF 2020: CP-3151. PREVIOUS REGISTRATION NUMBERSDR 2021F00369Indicator · failedLEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED WITH FLAP ASYMETRY BETWEEN FLAP UP AND FLAP ONE.SDR SWAA2022012451317Intercostal · crackedSUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 46 BS 328+7 WL 208. ; / [01] REMOVED AND LOCATED HOLES IN NEW INTERCOSTAL; AN INSTALLED AT BS 328+7 LBL 46 WL 208 PER SRM 51-40-02-0G-0;SRM 51-40-05-0G-0;DRAWING # 141A5400 SHT 44 REV -; [02SDR SCNA20211018084None · noneDEFECT: LANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF RESOLUTION: FOUND GROUND SPOILER INTERLOCK VALVE LOWER SLIDER ASSY. DISCONNECTED . CONEECTED LOWER SLIDER ASSY SLEEVE AND SAFTIED IAW AMM 27-62-51. ADJUSTMENT AND FUNCTIONAL CHECK GOOD . ACCOMPLISHED GSDR SCNA20210915081Support · corrodedCORROSION FLOOR TO SIDEWALL SUPPORT (ZEE CHANNEL) BS 500G + 11 TO 500I RBL 25.CORROSION ON SIDEPLATE 519-500G-500I RBL 23 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLD IAW SRM 53-00-53-IA-2 DERAIL "D" REV 73. REMOVED AND REPLACED SIDEPLATE WITH SDR SCNA20210915080Frame Angle · crackedANGLE ON FWD SIDE OF FRAME IS CRACKED BS 500D LBL 25 CARGO FLOOR. CRACK ON ANGLE FWD OF FRAME 500D LBL 25 FOUND TO BE OUT OF LIMITS IAW 5RM53-00-53-1A-2 REV 73. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-06-0 REV 73, BOEING DWG 143A7505 REV A.SDR SCNA20210915079Web · damagedE&E BAY DOOR CUTOUT L/H WEB IS DAMAGED. REMOVED DAMAGE E+E BAY DOOR CUTOUT WEB CBS 323-351 LBL 15 IAW SRM 737-800 51-40-02-0G FABRICATED WEB OUT OF 7075T6 .040 LOT # 5105057-1 ALODINE AND PRIMER NEW WEB IAW SRM 52-10-13-2A-3 REV 73 AND DRAWING PL141A8512 REV ESDR SCNA20210914078Baffle · crackedBAFFLE CRACKED BETWEEN BS 500C AND 500D LBL25 STRINGER 26 L/H. CRACK BAFFLE 500C AND TO 500D LBL25 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REV. 73, REMOVED AND REPLACED BAFFLE IAW SRM 51-40-02-06-0 REV 73, BOEING DWG 143A7505 REV A.SDR SCNA20210927082None · noneCORROSION FLOOR TO SIDEWALL SUPPORT (ZEE CHANNEL) BS 500G +11 TO 500I RBL 25. CORROSION ON SIDEPLATE STA. 500G-500I RBL 25 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE IAW SRM 53-00-53-1A-2 DETAIL "D" REV 73. REMOVED AND REPLACED SIDEPLATE WITH SDR 2021F00258Fitting · crackedDURING DETAILED INSPECTION WAS FOUND FRAME FITTING LH AND RH SIDE WITH CRACK AT STA 663.75. INSPECTION COMPLIED AS PER FAA AD 2021-09-06.SDR SCNA20210708076Gasket · failedDEFECT: GROUND CREW REPORTS FLAMES AND SMOKE FROM #1 ENG TAILPIPE ON SHUTDOWN - ACTION TAKEN: GAINED ACCESS TO OIL INLET COWL REPLACED PRECATUATIONARY FLANGE ASSY GASKET RAN ENGINE ON TO TAKE OFF POWER FOR 5 MIN AND LEAVES NOTED TO SUPPLY AND SCAVENGE AND SURRSDR SCNA20210618075Skin · damagedDAMAGE TO L/H O/B FLAP UNDER I/B FAIRING. REPAIRED 2.2"X1.5" GOUGE TO L/H O/B FLAP UNDER I/B FAIRING IAW B737-800 SRM 51-70-10-2R4 REPAIR 4& B737-800 SRM 5170-102R-0 REPAIR GENERAL. RESTORED FINISH IAW B737-800 AMM 51-21-73-370-803.SDR SCNA20210618073Support · corrodedFWD CARGO RH FLOOR TO SIDEWALL SUPPORT HAS SIGNS OF CORROSION FROM STA 500E TO 500G. REMOVED AND REPLACED FWD CARGO R/H FLOOR TO SIDEWALL SUPPORT PER B737-800 SRM 51-40-02- ON BS 500B TO 500I.SDR SCNA20210618072Support · gougedGOUGE ON LOW SURFACE OF SEAL SUPPORT ASSEMBLY AT RIGHT HAND SIDE WING,INBOARD FLAP,INBOARD SIDE BY A FUSELAGE. REMOVED AND REPLACED SEAL SUPPORT ASSEMBLY AT R/H SIDE WING PLATE PER B737-800 SRM 51-40-02.SDR SCNA20210618071Support · gougedLEFT HAND SIDE WING,SEAL SUPPORT ASSEMBLY HAS GOUGE ON LOW SURFACE LOCATED INBOARD FLAP AT INBOARD SIDE BY THE FUSELAGE. REMOVED AND REPLACED SEAL SUPPORT ASSEMBLY AFT L/H SIDE WING PLATE PER B737-800 SRM 51-40-02.SDR SCNA20210618068Support · crackedA CRACK APPROXIMATELY 3/4 INCHES UNDERNEATH A WEATHER RADAR SUPPORT FLATFORM AT RIGHT SIDE IN EE BAY JUST FWD OF EE BAY DOOR. REPAIRED WEATHER REDAR SUPPORT PLATFORM IN EE BAY IAW B737-800 SRM 51-20-13-2R REP. 1.SDR SCNA20210618074Panel · cracked6" CRACK ON BOTTOM SIDE OF PANEL 661AB. ONE PUNCTURE ON BOTTOM SIDE OF 661AB MEASURING 1"X1" AND A 1"X .5" GOUGE. REPAIRED 6" CRACK 1"X1" PUNCTURE AND 1.5"X.5" GOUGE ON BOTTOM SIDE OF PANEL 661AB IAW B737-800 SRM 51-70-04 REPAIR 11 AND SRM 51-70-04 REPAIR 2.SDR SCNA20210618067Skin · dentedFOUND DENT IN AFT CARGO DOOR DENT IS 2" LONG BY 1" WIDE AND .070" DEEP. REMOVED AND REPLACED AFT CARGO DOOR EXTERIOR SKIN FOR B737-800 SRM 51-40-02.SDR SCNA20210618066Structure · damaged#1 ENG R/H T/R AT NAS STA 235 AND WL 73" HAS BURN MARK. REPAIRED #1 ENG R/H T/R AT NAS STA 235 AND WL 73" IAW B737-800 SRM 51-70-08, PARA. 3., A,-6. RESTORED PAINT FINISH IAW 51-21-44-300-802 PARAGRAPH 3C(1)(A-C) AND AMM 51-21-73 PARAGRAPH E.SDR SCNA20210618070Doubler · gougedTHERE IS GOUGE ON A DOUBLER AT FWD OF RIGHT SIDE OF PANEL 192CR-2 LOCATED BOTTOM SIDE FUSELAGE,AIR CONDITIONING BAY AREA. REMOVED AND REPLACED DOUBLER AT FWD R/H OF PANEL 192CR-2 PER B737-800 SRM 51-40-02.SDR SCNA20210618069Panel · crackedFIBERGLASS PANEL HAS 2 CRACKS,ONE IS APPROXIMATELY 3" AT UPPER JUST ABOVE A LEFT HAND KEEL BEAM AND OTHER IS APPROXIMATELY 4" ADJACENT TO KEEL BEAM LOCATED LEFT MAIN WHEEL WELL FWD. REPAIRED 2 4" CRACKS ON VAPOR BARRIOR WEB PN:111A1141 IAW B737-800 SRM 57-10
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