Boeing 737-8KN
Service difficulty reports · 155
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 = '7378KN' 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 = '7378KN' 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 SCNA20240717277Spar · crackedCRACK ON OUTBD ANGLE AT RH WING FIXED TRAILING EDGE REAR SPAR APPROX WS 278.00. REPLACED PER B737-800 SRM 51-40-02-0G-0SDR SCNA20240717276Angle · crackedCRACKED ANGLES ON DOOR COVER 834DZ AND 844DZ. REPLACED PER B737-800 SRM 51-40-02-0G-0 PAR 4SDR SCNA20240717280Tee Angle · crackedCRACK IN TEE ANGLE OF BELLY FAIRING ACCESS PANEL 192CR SUPPORT AT STA 649.96. REPLACED PER B737-800 SRM 51-40-02-0G-0SDR SCNA20240422194Holder · loose1LN DOOR GIRT BAR HOLDER IS LOOSE. MX NOTIFIED. ADJUSTED CLAMP ON GIRT BAR HOLDER IAW AMM 25-64-00 MX NOTIFIEDSDR SCNA20240411192Door Sill · damagedON PRE-FLIGHT FOUND DAMAGE @ AFT CARGO DOOR LOWER CUT OUT SILL. REMOVED AND INSTALLED NEW MODIFIED SCUFF PLATE ON AFT CARGO DOOR LOWER CUT OUT SILL.SDR SCNA20240318158Oven · smokeAFT RIGHT OVEN SMOKING BADLY AND BLACK AND HOT AT TOP RIGHT GASKET. REMOVED AND REPLACED OVEN IN REF. TO AMM 25-30-61. OPS CHECK GOOD.SDR SCNA20240116007Light · unknownDEFECT: W/O 84120 NRC00007 R1 DOOR OUTSIDE EMER LIGHT IS BURNED OUT. - - RESOLUTION: RELAMPED R1 EXTERIOR EMERGENCY LIGHT. IAW AMM 33-51-04. OPS CHECK GOOD.SDR SCNA20231129240Unknown · unknownDEFECT 761004 - PHOTOLUMINESCENT STRIP LOOSE AT ROWS 11 & 12ABC. - RESOLUTION: RE-ATTACHED PHOTOLUMINESCENT STRIP AT SEAT ROWS 11 & 12ABC REF AMM 33 51-15SDR SCNA20231030241Unknown · unknownWO 82545 // TASK CARD: L1 DOOR AFT GIRT BAR LATCH HAS SHEARED RIVETS. REPLACED SHEARED L1 AFT GIRT BAR RIVET REF SRM 51-40-02SDR SCNA20231030240Unknown · unknownR2 DOOR AFT GIRT BAR LATCH HAS SHEARED RIVETS. REPLACED SHEARED R2 GIRT BAR LATCH RIVET REF SRM 51-40-02SDR SCNA20231205246Unknown · unknownWO 82424 NRC00003 - DURING EMERGENCY LIGHT CHECK FOUND RT FWD OVERWING FLOOR EXIT SIGN NOT WORKING. TRIED RELAMP, NO FIX. FURTHER TROUBLE SHOOTING REQUIRED FOUND CONNECTOR NOT FULLY INGAGED, RECONNECTED NOW LIGHT WORKS NORMAL.REF AMM 33-53-01SDR SCNA20230828212Unknown · unknownDEFECT 760547: 14A EMERGENCY EXIT LIGHT REMAINS ILLUMINATED - - - RESOLUTION: OPS CHECK GOOD IAW AMM REF 33-51-04 NO DEFECTS NOTEDSDR SCNA20230522160Slide · dislodgedDEFECT 769504: DOOR 2L SLIDE FELL OUT OF HOLDER. NO DEPLOYMENT OF SLIDE. - - - RESOLUTION: REINSTALLED SLIDE IN COVER AND INSTALLED ON DOOR PER AMM 25-66-01 INSPECTED INSTALLATIONS OF 2L DOOR SLIDE PER AMM 25-66-01SDR SCNA20230530166Floorbeam · corrodedDEFECT NR00303: FLOOR BEAM AT STA 344 LBL 10 SRM REPAIR MODIFICATION. - - - RESOLUTION: REMOVED EXISTING REPAIR AND MODIFIED FLOOR BEAM AT STA 344 LBL 10 TO COMPLY WITH SRM 53-10-51-2R-10 REPAIR.SDR SCNA20230509144Baffle · crackedDEFECT NR00272: FWD CARGO COMPARTMENT BAFFLE AT BS 500G - 500H LLBL 24 WL 160 CRAKCED.- - - RESOLUTION: REPLACED BAFFLE AT BS 500G - 500H LBL 24 WL160 PER B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A7505.SDR SCNA20230515153Intercostal · damagedDEFECT NR00269: DAMAGE FOUND ON INTERCOSTAL @STA 294.5+12 LBL 11, WL 208. - - - RESOLUTION: REMOVED AND REPLACED INTERCOSTAL AT STA 294.5+12 LBL 11, WL 208 IAW B737 SRM 51-40-02-0G AND DWG 141A5600SDR SCNA20230531172Intercostal · corrodedDEFECT NR00228: CORROSION ON FLOOR BEAMAT STA 344 LBL10 APPROX. - - - RESOLUTION: AFTER FURTHER INVESTIGATION FOUND CORROSION TO BE OUT OF LIMITS ON FLOOR BEAM AT STA344 LBL 10 APPROX INSTALLED A REPAIR IAW ER 23-10-01666 REV IR ENG-53SCA-11146-REV00. REPLACEDSDR SCNA20230515147Unknown · unknownDEFECT: NR00229: CORROSION ON FLOOR BEAM AT STA 294 LBL 10 APPROX (MARKED). - - - RESOLUTION: REPAIRED FLOOR BEAM AT STA 294 LBL 10 IAW B737 SRM 53-10-51-2R-14. REPAIR IS A CAT-A REPAIR.SDR SCNA20230512146Unknown · corrodedDEFECT NR00222: L2 MOP SEAL HAS AREAS OF CORROSION (MARKED). - - - RESOLUTION: EVALUATED CORROSION ON MOP SEAT L2 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED MOP SEAL PER B737-800 SRM 51-40-02-0G AND DWG #147A8501 REV B. SRM REF 53-70-15-1A-1. CAUSE OF CORSDR SCNA20230517154Shield · corrodedFWD CARGO BAY ON RH SHIELD HAS SIGNS OF CORROSION AROUND FASTENER HOLES AT STA 500 TO 500A. REMOVED AND REPLACED NEW SHIELD REPLACEMENT, PART # 143A8126, ON FWD CARGO BAY RH STA 500 TO 500A PER B737 SRM 51-40-02, SRM 51-40-05 AND BOEING DWG 143A008 REV - AT SDR SCNA20230515152Baffle · crackedDEFECT NR 00187: FCB HAS CRACKED BAFFLE CLIP AT STA 500G FWD L/H SIDE BL 24 (MARKED) - - -RESOLUTION: REMOVED AND REPLACED BAFFLE CLIP AT STA 500G FWD L/H BL 24 IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG #143A7505 ID 109.SDR SCNA20230508143Web · corrodedFWD CARGO BAY THRESHOLD WEB AT DOOR HAS EVIDECE OF CORROSION AROUND FASTENER HOLES 9. CORROSION DAMAGE ON FWD CARGO BAY THRESHOLD WEB AT DOOR EVALUATED AND FOUND TO BE OUT OF LIMITS PER B737 SRM 53-30-15-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED THRESHOLD WSDR SCNA20230518156Floorbeam · corrodedDEFECT NR00158: CORROSION ON 986 FLOOR BEAM UPPER SURFACE RBL 44. - - - RESOLUTION: REPAIRED BS 986 FLOOR BEAM UPPER CAP IAW SCA ENG-53SCA-11180 REV 00 AND ATS ER/A 23-01523 REV IR. CAUSE OF CORROSION: MOISTURE.SDR SCNA20230517155Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER SURFACE LBL 44. REPAIRED BS 986 FLOOR BEAM UPPER CHORD PER B737 SRM 53-70-51-2R-4 LBL 50 TO RBL 11. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS PER B737 SRM 53-70-51-1A-1 PARA. 4 H (2),(B)(1) FIG 104 DETAIL C. CAUSE OF CORROSIOSDR SCNA20230328114Unknown · unknownDEFECT 684679: DURING APPROACH TO LANDING THE AMBER L/E FLAP TRANSIT LIGHT ILLUMINATED AND STAY ILLUMINATED PERFORMED QRH AND LANDED FLAPS 15 NORMALLY. RESOLUTION: BITE FSEU CURRENT FAULT 27-81354. PER FIM 27-81 TASK 806 CYCLED C/B'S FLIGHT CONTROL FSEU DC 1SDR SCNA20230328116Unknown · unknownDEFECT 744805: TRAILING EGDE FLAPS DISAGRE INFLIGHT. FLAP HANDEL AT 30; FLAPS INDICATED JUST OVER 25 . FLAPS DID NOT MOVE UP WHEN SELECTED INFLIGHT BUT DID MOVE TO 30 AFTER LANDING. (EMERGENCY DECLARED, LANDED SAFELY) - - - - - RESOLUTION: TROUBLESHOOTING SHOWSDR SCNA20230313099Unknown · unknownDEFECT: TRAILING EGDE FLAPS DISAGRE INFLIGHT. FLAP HANDEL AT 30; FLAPS INDICATED JUST OVER 25 . FLAPS DID NOT MOVE UP WHEN SELECTED INFLIGHT BUT DID MOVE TO 30 AFTER LANDING.: RESOLUTION: TROUBLESHOOTING SHOWED FAULTY L/H FLAP POSITION TRANSMITTER.R&R'D L/SDR SCNA20230221083None · noneDEFECT W/O 76727 NR00001: L1 SLIDE COVER WINDOW FOR BOTTLE PRESSURE GUAGE INSPECTION IS CRACKED. RESOLUTION: REMOVED AND REPLACED L1 DOOR SLIDE WINDOW. SLIDE IS REMOVED FROM AIRCRAFT AND NEEDS TO BE REINSTALLED WHEN WINDOW SEALANT IS DRY..
REF AMM 25-66-01-SDR SCNA20230130047Door · openEXTERNAL GROUND POWER DOOR WAS LEFT OPEN. VIBRATIOIN AND BUZZING NOISE OBSERVED DURING FLIGHT. INSPECTED EXTERNAL GROUND POWER DOOR IAW AMM 52-49-02-400-801 OPERATIONAL CHECK GOOD. A/C OK FOR CONTINUED SERVICESDR SCNA20230125045Lamp · inoperativeL2 EXTERIOR EMERGENCY LIGHT INOP RELAMPED EXTERIOR L2 EMERGENCY LIGHT. OPS CHECKED GOOD. REF AMM 33-51-00.SDR SCNA20230117041Pump · low pressureHYDRAULIC SYSTEM A ENGI 1 LOW PRESSURE LIGHT IILLUMINATED FOLLOWED BY LOSS OF HYDRAULIC GUQNTITY IN FLIGHT IN SYSTEM A. RAN QRH AND LANDED UNEVENTFULLY OVERWEIGHT. REMOVED AND REPLACED #1 ENG HYD PUMP PER AMM 29-11-400-801-001 AND 29-11-11-000-801-001. REPLSDR SCNA20230113040None · noneFUEL SMELL NOTED IN PAX CABIN AS CREW ENTERED AIRCRAFT : RESOLUTION: GASOLINE SMELL WAS NOTED PRE TAXI. AUTO FUEL SMELL WAS ATTRIBUTED TO GAS POWERED HEAT CART PREVIOUSLY ATTACHED TO A/C.SDR SCNA20230130050Sight Glass · missingL2 EMERGENCY SLIDE SIGHT GLASS MISSING. FOUND SIGHT GLASS AND RESECURED. REF AMM INTRODUCTION NR 2. OK FOR SERVICESDR SCNA20230103001Flap System · faultedFLAPS WOULD NOT DEPLOY NORMALLY. SELECT FLAPS 1 BUT REMAINED UP. USED ALTERNATE EXTENSION PROCEDURE AND LANDED WITH FLAPS 15. ACCOMPLISHED T/E FLAP SYSTEM TEST IAW AMM 27-51-00-730-801 AND NO FAULTS NOTED. ACCOMPLISHED FSEU BITE TEST PER FIM 27-51 TASK 8SDR SCNA20221122147Girt Bar · out of positionESCAPE SLIDE EXTENDS TOO FAR FROM DOOR L2. REPOSITIONED GIRT BAR AS TO PROPERLY STOW .REF AMM 25-66-01.NOTE: DID NOT REMOVE SLIDE OR OPEN COVER TO ACCOMPLISH.SDR SCNA20221020134Light · noneDEFECT WORK ORDER 74336 NR00001: DURING EMERGENCY OPS CHK FOUND LEFT AFT OVERWING LIGHT INOP. RESOLUTION: R & R LEFT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHK GOOD.SDR SCNA20220831102Controller · failedDEFECT 700594: DURING DESCENT CABIN ALTITUDE UNCONTROLLABLE. RAN QRH 2.4 SWITCHED TO ALT, NO CHANGE. SWITCHED TO MAN AND OPENED OUTFLOW MANUALLY. RESOLUTION: FOUND FAULT 42 ON CPC #2 REMOVED AND REPLACED #2 CABIN PRESSURE CONTROLLER OPS CHECK GOOD REF AMM 2SDR SCNA20220805091Bracket · bentDEFECT: FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR RETAINER BRACKET ON SIDE COVER BENT. RESOLUTION: REMOVED AND REPLACED 1L DOOR EMERGENCY SILDE COVER ASSY. REF AMM 25-66-01SDR SCNA20220718082Slide · failed inspDEFECT: 1L GIRT BAR LOOSE - SLIDE FELL OFF WHEN OPENING. RESOLUTION: GIRT BAR RESECURED REF AMM 25-66-00. OK FOR SERVICE.SDR SCNA20220617071Girt Bar · looseDEFECT 681739: 1R GIRT BAR HOUSING BRACKET IS NOT SECURE RESOLUTION: REMOVED SLIDE FROM R1 DOOR TO FOM AND RESECURED GIRT BAR HOUSING BRACKET. THEN REINSTALLED SLIDE ON R1 DOOR REF AMM 25-66-01. RII ACCOMPLISHED BY 31619SDR SCNA20220523050Flap System · asymetricDEFECT: HAD A FLAP ASYMMETRY WHEN EXTENDING TO THE FLAPS 1 POSITION (ON TRAILING EDGE FLAPS). RESOLUTION: REPLACED FLAP POSITION INDICATOR REF AMM 27-58-02. OPS CHK GOOD.SDR SCNA20220325015Cover · missingDEFECT: LIGHT COVER NEAR AFT LEFT LAV IS MISSING. RESOLUTION: INSTALLED ADT LEFT ASSY LENS IAW B737 AMM SCA D633A101-SCA TASK 33-57-14-960-802SDR 2022FA0000059None · noneCORROSION ON SHIELD AT BS 492-500A STRINGER 26R/H. REPLACED SHIED AT B.S. 492-500A STRINGER 26 R/H PER DRAWING 143A0080 I.A.W B737 SRM 51-40-02-0G-0 RU74, B737 SRM 51-40-05-0G-0 REV 74.SDR 2022FA0000058None · noneLIGHTNING STRIKE IN FUSELAGE SKIN @STA. 277, 1.5" ABOVE STR. 16R. REMOVED DAMAGE AT BS 277 1.5" ABOVE STR
16R IAW B737-800 53-00-01 REPAIR 36 REV 74 CUT OUT MEASURES 1.00" WIDE BY 4.00" LONG. FABBED DOUBLER FROM .040" 2024-T3, TRIPLER FROM .063" 2024-T3 AND FSDR SCNA20211020086Light · failedSMOKE STARTED COMING OUT OF CA YOKE FLIGHT NUMBER BACK LIGHTING FOR A VERY BRIEF PERIOD OF 3- 5 SECONDS BACKLIGHTING IS NOW INOP AS WELL AS THE BACKLIGHTING ON CA SIDE LOWER LIGHTING RHEOSTAT KNOBS + FMC ACARS BACKLIGHTING R&R CA MEMORY LIGHT ASSY IN REFERESDR SCNA20210528059Panel · damagedL/H L/E WING PANEL 521JB HAS TWO EA. DAMAGED FASTENER HOLES. REPAIRED 2 EA. DAMAGED FASTENER HOLES ON L/H L/E WING PANEL 521JB. IAW B737 SRM 57-41-01-2R-1 AND B737 SRM 51-70-05-2R-9.SDR SCNA20210528058Panel · damagedR/H WING L/E PANEL 621YB HAS ELONGATED FASTENER HOLE. REPAIRED ELONGATED FASTENER HOLE ON R/H WING L/E PANEL 621YB. IAW B737 SRM 57-41-01-2R-1 AND B737 SRM 51-70-05-2R-9SDR SCNA20210528062Skin · dentedLEFT HAND WING #3 SLAT UPPER SURFACE HAVE A DENT 51" FROM OUTBOARD AND 3" FROM TRAILING EDGE. REPAIRED DENT AT 51" FROM OUTBOARD AND 3" FROM TRAILING EDGE ON LEFT HAND WING #3 SLAT UPPER SURFACE IAW B737 SRM 57-42-01-2R-11 + SRM 51-70-10-2R-2.SDR SCNA20210528061Skin · dented#5 SLAT UPPER SURFACE HAVE A DENT LOCATED 3.750" FROM TRAILING EDGE AND 3" FROM OUTBOARD EDGE. REPAIRED DENT LOCATED 3.75" FROM TRAILING EDGE AND 3" FROM OUTBOARD EDGE ON #5 SLAT UPPER SURFACE PER 737-800 SRM 57-42-01-2R-11 AND SRM 51-70-10-2R-2.SDR SCNA20210528057Panel · damagedR/H WING L/E PANEL 621QB HAS EXPOSED COMPOSITE ON EXTERIOR SURFACE. REPAIRED DAMAGED COMPOSITE ON EXTERIOR SURFACE ON R/H WING L/E PANEL 621QB IAW SRM 57-41-01-2R-1 AND SRM 51-70-05-2R-10.
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