Boeing 737-900ER
Service difficulty reports · 1,008
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 = '737900ER' 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 = '737900ER' 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 CALA2023031700789Skin · crackedRH HORIZONTAL STAB LOWER SKIN CRACKED 1" IN LENGTH AT APPROX STA 129.50 I/B OF THE 7TH DRAIN HOLE 17" FROM L.E.M REF BY AIRB ORNE/PEMCO NR.13619.0325 ACCOMPLISHED CUTOUT OF CRACK ON R/H HORIZ STAB LOWER SKIN @ APPR TO VERIFY ENDS OF 1.85"L CRACK & TO VERIFY CSDR DALA2023032002081Lens · missing(LOG 4098056) DURING INSPECTION FOUND EXIT" LIGHT COVER MISSING IN FRONT GALLEY. MAINTENANCE REPLACED LENS.SDR CALA2023031700772Unknown · damagedREF L/P4007970. LH HORIZONTAL STAB O/B L/E LOWER SPAR CHORD DAMAGED AT STA327 LOCKED FOR MX FERRY REF L/P4018513. REMOVED AND REPLACED LH HORIZONTAL STAB O/B L/E PHOTOS UPDATED. SKIN PICKED UP HOLES EXCEPT IN O/B END WHERE SPAR DAMAGE IS PRESENT, SPEED TAPED ASDR CALA2023031300722Unknown · unknownEMER EXIT LTS ON ROW 32 - ROW 35 REPLACED BATTERY PACK AND POWER SUPPLY M2626 AND OPS CK REF AMM 33-51-06-960-805 TESTS GOOD ADD EMP:U117464 ACP IDT INSPECTION OF EMERGENCY PATH LIGHTING OPERATION. CKS OK.SDR CALA2023031300719Tire · wornRH NOSE TIRE WORN TO LIMIT REQUIRES REPLACING. R/R RH NLG TIRE IAW AMM 32-45-21 PARTS USED: 1788932,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1788932 SN OFF 2069 WHEEL, ASSY, NL OFF 29-3245-9-0002 2069 ON 29-3245-9-0002 0294SDR DALA2023031501894Light · broken(LOG 9976720) DURING INSPECTION FOUND FWD GALLEY LOC 402 RED AND WHITE EMERGENCY LIGHT LENSES ARE BROKEN. INSTALLED NEW LIGHT ASSEMBLY REF B737 AMM 33-51. ALL CKS OK.SDR CALA2023031300714Engine · unserviceableDUE TO OIL CONSUMPTION TRENDS (RATE 0.67QPH AND CLIMBING) ON THE NO:2 ESN 658485, PLEASE BAG ALL DRAINS AND PERFORM PART POWER L EAK CHECK PER ENGINE VENTS & DRAINS INSPECTION IAW AMM 71-71-00 -200-801-F00 AND EXTERNAL OIL INSPECTION PER AMM 79-00-00-200-80 2SDR ASAA2023031042317Motor · noisyFOUND R/H #2 AFT FUEL BOOST PUMP MAKING LOUD / ODD NOISE. GROUNDED - YES. R/R #2 AFT FUEL BOOST PUMP PER B737-900 AMM 28-22-41.SDR ASAA2023031042307Power Supply · failedREF TC 78233001 - R AFT OVERWING ESCAPE LT, & AISLE LTS L1507, L1513, & L1517 FAIL CAPACITY CHECK - EMERGENCY BATTERY. GROUNDED - YES. REPLACED EMERGENCY EXIT POWER SUPPLY M1671 WITH SERVICEABLE UNIT OPS CHECKS OK. REF B737-900 AMM 33-51-06-960-806.SDR CALA2023031000686Tire · blownBLOWN TIRE ON TAKEOFF AS 160KTS TIRE SPEED 150KTS GEAR NEVER RET RACTED #2 TIRE BLOWN ON TAKE OFF. REMOVED AND REPLACED #2 MLG TIRE AS PER AMM 32-45-11. OK TO CONTINUE. PARTS USED: 60-3249-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1843117 SN OFSDR CALA2023030900663None · missingEMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - EMER PATHWAY LIGHTS AT SEATS 1ABC, 12ABC,20ABC & 23ABC INOP OR LENS MISSING. RELAMPED AND REPLACED LENS REF AMM TASK 33-51-11-960-801 OPS CHECKED GOOD. VERIFIED CORRECT LENS INSTALLATION AND OPS SDR DALA2023031301809Tire · failedSHIP 3906 -TIRE- #1 TIRE FAILURE DURING TAKEOFF. CORRECTIVE ACTION: TIRE REPLACED ON LOG PAGE 9921565.SDR CALA2023030900653Beam · corroded(B737-53-3-0737) MAIN CABIN FLOORBEAM UPPER SURFACE HAS CORROSION AT STA 947, RBL 50. TRANSCRIBED FROM HAECO GSO NRC# 9288446 REPAIRED FLOORBEAM AT STA 947 RBL 50 IAW B737 SRM 53-70-51-2R-5. INSP QC453 REMOVED AND REINSTALLED CREASE BEAM STIFFNERS FROM 927-96SDR CALA2023030900650Beam · corroded(B757-53-3-0737) MAIN CABIN FLOORBEAM UPPER SURFACE HAS CORROSION AT STA 947, LBL25. TRANSCRIBED FROM HAECO GSO NRC# 9288445 DAMAGE FOUND OUT OF LIMITS IAW B737-900ER SRM 53-70-51-1A-1 AND INSTALLED REPAIR IAW B737-900ER SRM 53-70-51-2R-5. HAECO GSO ME CH V8SDR CALA2023030300605Fastener · missingPDA 3 REPORTED BY RAMP. #6 CANOE FAIRING HAS SEVERAL FASTENERS MISSING. ADDED PHOTO. REPLACED 4 EACH SCREWS ON #6 FLAP TRACK FAIRING TAIL CONE. REF IPC 27-51-18-01. ITEM 435.SDR CALA2023030300616Seat Track · corrodedSUPPORT TASK: MAIN CABIN SEAT TRACK STA 500D-500E LBL24 HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC# 9288266 REMOVED CORROSION FROM MAIN CABIN SEAT TRACK STA 500D-500E LBL-2 HAECO GSO MECH V900579 INSP QC453 4, MAX ALLOWED IS .040, MATERIAL LOSS .080 OUT OFSDR CALA2023030300613Seat Track · corroded(SUPPORT TASK) MAIN CABIN SEAT TRACK STA 500D-500E LBL-45 HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC# 9288269 REMOVED CORROSION FROM SEAT TRACK STA 500D-500E LBL 45, MAX ALLO REPAIR 4. HAECO GSO MECH V900579 INSP QC453 WED LOSS .020, MATERIAL REMOVED .080SDR ASAA2023022842114Lamp · inoperativeEMERGENCY LIGHT BEHIND L2 DOOR NOT TURNING ON. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT BULB AFT OF L2 SERVICE DOOR REF AMM 33-51-04. OPS CHECK GOOD.SDR CALA2023022700570Speed Brake · noneSPEED BRAKE DO NOT ARM LIGHT ILLUMINATED WHEN THRUST LEVERS WERE ADVANECED FOR TAKEOFF UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V939727 FIM 27-62- TASK 802. ORTIZ, FABIO (V939727) PLEASE CONTACT TOMC BEFORE COMMENSDR CALA2023022700564Pseu · noneREJECTED TAKEOFF AT 110 KNOTS FOR TAKEOFF CONFIG LIGHT ILLUMINATED PILOT REPORTS WEIGHT 156,000 LBS. THRUST REVERSERS WERE ENGAGED. LIGHT MANUAL BRAKING. COULDNT DUPLICATE. NO RTO BRAKES. PERFORMED TROUBLESHOOTING PER FIM 31-51 TASK 803. FOUND ALL GOOD. REF ASDR ASAA2023022642101Regulator · faultyFLT CREW REPORTS WITH ALL BLEED VLVS. (APU & #1 & #2 ENGS) R2 DUCT PRESSURE READS 20PSI ALL BLEEDS OFF. GROUNDED - YES. REMOVED AND REPLACED BLEED AIR REGULATOR REF B737-900 AMM 36-11-03 UP TO STEP 3.E.(6). PERFORM LEAK & OPS CHECK ON #2 ENGINE REF. B737-900 FSDR DALA2023022701438None · none(LOG 4105765) DURING INSPECTION FOUND CORROSION AROUND BELLY DRAINS AT STATIONS 420,460,480,500A,500B,500D,500I AND 500U. CORROSION CORRECTED ON ELECTRONIC NON ROUTINE CARDS 1,2,3,4,5,6,7 AND 8 PER B737 SRM 53-30-01.SDR CALA2023022700549Skin · gougedRH FUSE SKIN IS DEEPLY GOUGED JUST AFT OF RH HORIZONAL STAB UPR MOVEABLE SEAL TRACK. GRID MAPPED DAMAGED AREA. LENGTH AND WIDTH ARE 1.00" X 0.50" BLENDED DAMAGED AREA. REF SRM 53-80-01. ACP''D HFECPER NDT PT6, 51-00-00-23, NO CRACKS NOTED. AND MAX DEPTH IS 0SDR DALA2023022401405None · noneSHIP 3911 -DIV- DIVERTED TO BOI DUE TO ODOR IN THE CABIN. CORRECTIVE ACTION: FOUND DE-ICE FLUID IN HEAT EXCHANGER PLENUM. REMOVED SAME. REPLACED RECIRCULATION FILTERS. NO FURTHER ODOR. AIRCRAFT RETURNED TO SERVICE.SDR CALA2023022400548Door · out of balanceFA REPORT LOUD AIR/PRESS URE LEAK ON DEPARTURE AT DOOR 1L H INSIDE AND OUT (VERY AUDIBLE). REF AMM 05-51-91.ALSO FOUND U PPER GUIDE ARM JAM NUT LOOSE.SUSPECT DOOR OUT OF RIG/ALIGNMENT REF AMM 52-11-00-820-801. PERFORMED INSPECTION OF DOOR 1L REF AMM 52-11-00,SDR CALA2023022400524None · corrodedCORROSION ON FLOOR ANGLE FROM STATION 860-867, RBL 54. REF NON-R OUTINE 001210079 REPAIR ACCOMPLISHED SEE BAM NR#001210079...REF EC/RA 5311-02948. VERIFIED ABOVE INFORMATION.SDR CALA2023022400523None · corrodedCORROSION ON FLOOR ANGLE LOCATED AT STATION 867 LBL 54.REF BAM NON-ROUTINE 001210085 REPAIR ACCOMPLISHED SEE BAM NR#001210085...REF EC/RA 5311-02947. VERIFIED ABOVED INFO IS CORRECT. VERIFIED REPIAR IS COMPLETE PER ECRA 5311-02947SDR CALA2023022400522None · noneCORROSION ON FLOOR BEAM ANGLE ADJACENT TO STATION 727F, LBL54 RE F BAM NON-ROUTINE 001210160. REPAIR ACCOMPLISHED SEE BAM NR#001210160...REF EC/RA 5311-02949. VERIFIED REPAIR.SDR CALA2023022200520None · noneRTO AT 90KTS DUE TO AFT LEFT ENTRY LIGHT ON T/O PERFORMED AFT ENTRY DOOR SYSTEM TEST REF AMM 52-13-00-700-805 TEST OK, INSPECTED DOOR FOR FLUSHNESS AND CLOSING OK, DOOR SEAL GATES OKSDR CALA2023022200513Skin · noneFUSELAGE SKIN REPAIR DOULBER INSTALLED AT STA 310 OVER STRINGER 21R. SEE BAM NON-ROUTINE 00122565 FOR INSTALLATION. PER SRM 53-0 0-01-2R-1 REPAIR 1 STEP 5 A DIP IS REQUIRED TO BE ISSUED. CYCLES AFTER REPAIR, WHICHEVER IS LATER. REPEAT INSPECTION AND PERFORM INSDR CALA2023022200512Floorboard · corroded(B737-53-3-0711) MAIN CABIN UNDER FLOORBOARD AT STA 328, APPROX RBL 10 HAS SURFACE CORROSION ON LATERAL I-BEAM TOP SURFACE AS MA RKED. TRANSCRIBED FROM HAECO GSO NRC# 9288423 CORROSION ON LATERAL I-BEAM TOP SURFACE AT STA 328 RBL10 WAS EV DAMAGE IS FOUND TO SDR CALA2023022000485Tire · noneLOW SPD ABORTD T/O. AT APPRX 60 KTS ACFT PULLD HARD TO LEFT. EN GNS SYSMTRCL. FULL T/S BRAKE DRAG WHILE MLG IS LIFTED. ROTATED TIRES AND FOUND ALL BRAKES OPERATING NORMALLY. NO DEFECTS FOUND. FURTHER TROUBLESHOOTING REQUIRED. PERFORMED LAND VERIFY TEST TEST SDR ASAA2023021841985Unknown · unknown#2 HF DISPLAYS "FAIL FAIL" APPROX 5 SEC AFTER TUNING A FREQ. GROUNDED - YES. COULD NOT DUPLICATE FAIL FAIL MESSAGE PERFORMED B737-900 FIM 23-11 TASK 806 OPS CHECK GOOD. ETOPS GROUND VERIFICATION CELL CALL SUCCESSFUL.SDR DALA2023022101276Lens · broken(LOG 2633010) DURING INSPECTION FOUND FWD ENTRANCE AISLE EEPL (RED AND WHITE) BROKEN. REPLACED FWD ENTRANCE AISLE EEPL (RED AND WHITE) IAW BOEING 737 AMM 33-51-14-960-801.SDR DALA2023022101275Lens · broken(LOG 2633004) DURING INSPECTION FOUND AFT R/H LAV EEPL (RED AND WHITE) BROKEN. REPLACED AFT R/H LAV EEPL (RED AND WHITE) IAW AMM B737 33-51-14-960-801.SDR DALA2023022101279Light · defective(LOG 9919160) DURING INSPECTION FOUND SEAT 19A OVERWING EXIT RED LIGHT ILLUMINATED. R/R LIGHT 10ABC AND PERFORMED PHASE II DATA LOAD. OPS CHK NML.SDR CALA2023021400442Flap System · inoperativeFLAPS DO NOT OPERATE WITH PRIMARY CONTROL EXTENDED NORMAL TO 5 WOULD NOT MOVE PAST 5 DEG. IN NRML MODE AL TERNATE WORKED OK REF FIM 27-51 TASK 801 FSEU BITE PROCEDURE GOT MSG 27-51427 SHOW,THEN THERE WAS AN INTERMITTENT FAULT.NO FURTHER FLAP LEVER .REF TASK SDR CALA2023021400438Skin · gougedRH FUSE SKIN IS DEEPLY GOUGED JUST AFT OF RH HORIZONAL STAB UPR MOVEABLE SEAL TRACK. GRID MAPPED DAMAGED AREA. LENGTH AND WIDTH ARE 1.00" X 0.50" BLENDED DAMAGED AREA. REF SRM 53-80-01. ACP''D HFECPER NDT PT6, 51-00-00-23, NO CRACKS NOTED. AND MAX DEPTH IS 0SDR CALA2023021300430Hmu · faultyRTO BELOW 80 KTS DUE TO 1 ENGINE NOT PRODUCING REQ. THRUST WITH A/T AND MANUAL MONITORING CHANGES TO REGULATOR -9. REF FIM 73-05-TASK808, ACPD #1 ENG EEC BITE, NO FAULTS NOTED, ACPD #1 ENG EEC ACT TEST, NO FAULTS, STARTED #1 ENG-IDLE, HAD REGULATOR 9 ON INPUTSDR CALA2023021300429Unknown · noneOIL FILTER BYPASS MSG DURING FLT. COMPLETED REMOVED 3 EA. MCD TO INSPECTOR CHIP DETECTORS AND SCAVENGE RE-INSTALED 3EA. MCD. REF. AMM TASK 79-21-05-400-804-F00. PART USED FOR MCD IS 29-7921-3-0034, 3EA. VERIFIED NEW FILTERS INSTALLED. PERFORMED OIL SUPPLY FILTSDR CALA2023021300425Unknown · crackedLOWER FUS.CENTER WING BOX CTR BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ APPROX. LBL6, STA 663.75 REF. AAR N/R:9515623. REPAIRED WING CENTER BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE LBL 6, STA 663.75SDR CALA2023021300424Unknown · crackedLOWER FUS.CENTER WING BOX CTR BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ APPROX. RBL6 , STA 663.75 REF. AAR N/R:9515625 REPAIRED WING CENTER BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE RBL 6, STA 663.75.SDR CALA2023021300423Skin · missingPDA 2 FOUND DAMAGE TO RIGHT WING OUTBOARD TRAILING EDGE FLAP. ALUMINUM SKIN MEASURING APROX 22" X 12" DETACHED FROM LOWER TE FLAP. DAMAGED RH TRAILING EDGE FLAP REPLACED. PARTS USED: 29-5753-9-0010,QTY :1 1072614,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - SDR CALA2023021300412Angle · unknownMRD BROKEN MRD *EWR 01-2019Z* FOR AIRCRAFT 0419 BROKEN ON 01FEB23 17:10:45 ON FLIGHT 1340 FROM EWR TO DEN. REASON: LOG PAGE 3741587 CREATE D NO FURTHER MAINTENANCE ACTION NEEDEDSDR CALA2023021000378Flap System · warning lightTRAILING EDGE FLAPS DISAGREE WITH POSITION HANDLE AT 30 BUT INDI CAT ING FLAPS 5 CYCLED FLAPS SEVERAL TIMES, PASSED FSEU BITE PER 27-51 TASK 801, ACCOMP VISUAL INSPECTION OF FLAP OPERATON. CAN NOT DUPLICATE, OK PER TSM 27-51 TASK 802.SDR CALA2023021000402Angle · crackedLOWER FUS.CENTER WING BOX CTR BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ APPROX. RBL6 , STA 663.75 REF. AAR N/R:9515625 REPAIRED WING CENTER BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE RBL 6, STA 663.75 PER REF.B737 SRM 57-10-10- 2R-5,RSDR CALA2023021000401Angle · crackedLOWER FUS.CENTER WING BOX CTR BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ APPROX. LBL6, STA 663.75 REF. AAR N/R:9515623. REPAIRED WING CENTER BULKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE LBL 6, STA 663.75 PER REF.B737 SRM 57-10-10- 2R-5,RESDR CALA2023021000397Suppression Sys · unserviceableTRANSFERRED FROM HAECO LOG PAGE 9288151. LOG CREATED FOR SDR REPORT ONLY. RT WING TRAILING EDGE REAR SPAR STA 261, #2 ENG FIRE SUPRESSION TUBE SHEARED AT COUPLING.SDR ASAA2023020841908Regulator · failed"BLEED TRIP OFF" ON DEPARTURE, CLIMBING THROUGH 12,000. RAN QRH PROCEDURE."TRIP RESET " DID NOT RESET. GROUNDED - YES. AIR TURNBACK -- REMOVED AND REPLACED PRSOV B737-900 AMM 36-12-02. REMOVED AND REPLACED HIGH STAGE REGULATOR AMM 36-11-07.SDR DALA2023020901049Lens · broken(LOG 9455604) DURING INSPECTION FOUND RED COVER OVER EXIT LIGHT NEAR 2R LAV BROKEN. ROBBED PN: 81000-6085ATS FROM 3862. IAW SWPM 20-30. OPS CHECK NORMAL.
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