Boeing 737-9
Service difficulty reports · 3,497
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 = '7379' 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 = '7379' 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 ASAA2023072444213Unknown · unknownFMC DISAGREE. GROUNDED - YES. PERFORMED GOOD OPERATIONAL TEST OF FMC REF AMM 34-61-00-710-801.SDR ASAA2023072444202Unknown · unknownFOUND AMBER MAINT LIGHT ON. GROUNDED - YES. STATUS PAGE SHOWING: ENG 1 FAN COMP OVHT SENSOR, ENG 1 CONTROL, ENG 1 REVERSER. FOUND P91 MAINT S/W ENABLE, AND EEC 1 IN TEST MODE. ACCOMPLISHED IFIM TASK G73-20-00-810-869. NO FAULT HISTORY OR CORRELATED MSG. EEC1 MSDR DALA2023072505969Unknown · unknown(LOG 2882419) FWD CARGO BAY R/H AFT SHIELD IS CORRODED (MARKED). STA 500-500B; RBL 36, WL 156. REMOVED AND REPLACED FORWARD CARGO AFT SHIELD IAW B737 SRM 51-40-02, B737 SRM 51-40-05 AND BOEING DRAWING# 143A8126.SDR ASAA2023072344167Unknown · unknownWHILE PERFORMING , T/C 31-005-00 W/O 1962050. FOUND "ENG 1 EEC C2" MSG ON SCHEDULE MAINTENANCE TASK DISPLAY SYSTEM. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072344158Unknown · unknownWHILE PERFORMING T/C 31-005-00 FOUND LONG TIME FAULT "ENG 2 EEC C2" ON SCHEDULED MAINTENANCE TASK DISPLAY SYSTEM. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072344148Unknown · unknownPER T/C 31-005-00 FOUND LATCHED MESSAGE PACK CONTROL CHANNEL R. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072344206Unknown · unknownAPU LOW OIL PRESSURE LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED IFIM TASK 49-10-00-810-801 STEP B. INITAL EVALUATION. NO FAULTS FOUND. APU OPS NML. SEAMC ROBERT NOTIFIED. A/C OK FOR SERVICE.SDR ASAA2023072344200Unknown · unknownDURING THE DESCENT CHECK LIST- ON "RECALL" MASTER CAUTION AND "SPEED TRIM LIGHT" ILLUMINATED, RAN QRH- BOTH LIGHTS EXTINGUISHED THEN MASTER CAUTION SYSTEM WAS RESET. GROUNDED - YES. CW IFIM 22-11-00-810-D71 MAINTANCE MESSAGES 22-11Q16 AND 22-11822 BITE TEST PASDR ASAA2023072344199Unknown · unknownAUTOPILOT REVERTED TO CWS IN PITCH /ROLLWITH VNAV/LNAV DISENGAGING TWO TIMES UNCOMANDED. BOTH TIMES RESET TO NOM OPS. GROUNDED - YES. PERFORMED IFIM 22-11-00-810-D20 ND IFIM 22-11-00-810-D21. NO ACTIE FAULTS. ONLY DFCS SHOWED RT FMC INTERMITTENT NO INFO FOM ADSDR ASAA2023072244211Modulating Valve · faultyTECH SERVICES REQUEST FOR FOLLOW-UP TO MTX LIGHT & FAULT(#1 LEFT FAMV FAULT 36-12020 #1(LH) FAMV IS NOT IN COMMANDED POSITION)----(#PRI1)----ETOPS SIGNIFICANT SYSTEM----. GROUNDED - YES. (RESOLVED ON W/O: 1962416 TASKCARD: N/R-00002 ) REMOVED AND REPLACED #1 LSDR DALA2023072505972Unknown · unknown(LOG 2879135) RH HORIZONTAL STABILIZER REAR SPAR UPPER CHORD LOWER SURFACE HAS EVIDENCE OF CORROSION 21 FROM STABILIZER TIP. ACCOMPLISHED BLEND REPAIR IAW ER/A 610164-14 REV ORIG.SDR DALA2023072505968Unknown · unknown(LOG 2879269) CRACK SUPPORT ANGLE LOCATED BS 727 BTW STR 25R AND STR 25L AFT CARGO COMPARTMENT. COMPLIED WITH ER/A 610058-14 REV ORIGINAL.SDR ASAA2023072244175Valve · unknownWHILE PERFORMING NO1 ENG WASH T/C FOUND HPSOV OPEN/CLOSE LOCK BOLT HELICOIL CAME OFF. GROUNDED - YES. REMOVED AND REPLACED HPSOV WITH REF AMM 36-11-07. OPS CHECK GOOD.SDR ASAA2023072244173Unknown · unknownWHILE PERFORMING T/C 31-005-00 FOUND "BLEED FAMV RVDT R" FAULT SHOWING ON SCHEDULED MAINTENANCE TASK DISPLAY SYSTEM. GROUNDED - YES. ACCOMPLISHED R/H PNEUMATIC ELECTRICAL LRU- REPLACEMENT TEST REF AMM 36-00-00. TEST PASS. "BLEED FAMV RVDT R" FAULT NO LONGER ACSDR ASAA2023072244151Unknown · unknownFOUND LATCH FAULT PACK CONTROL CHANNEL R. GROUNDED - YES. FOUND FAULT CODE 21-55341 PERFORMED IFIM TASK 21-51-00 SEC B INITIAL EVALUATION TO STEP 3. THIS CLEARED LATCH MESSAGE PACK CONTROL CHANNEL R. NO FURTHER ACTIONS NEEDED.SDR ASAA2023072144168Unknown · unknownSMT MSG ENG 1 EEC C2 FAULT. GROUNDED - YES. ON DEFERRAL.SDR DALA2023072505967Unknown · unknown(LOG 2877179) FORWARD CARGO COMPARTMENT LH SIDE BS 500C FRAME HAS A DENT BETWEEN STRINGERS 25L AND STRINGER 26L. REMOVED DENT DAMAGE AND ACCOMPLISHED REPAIR ON FORWARD CARGO COMPARTMENT LH SIDE BS 500C FRAME BETWEEN STRINGERS 25L AND STRINGER 26L IAW B737 SRM SDR ASAA2023072144176Unknown · unknownAFTER LANDING GROUND 80 KNOTS "MAINT" LIGHT ILLUMINATED ON OVER HEAD PANEL. GROUNDED - YES. FOUND MAINTEANCE MESSAGE 36-12020 FOR FAMV ENGINE 1 PERFORMED PNEUMATICS ENGINE ON SYSTEM TEST PER REF AMM36-00-00-730-801. TEST PASSEDMAINT LIGHT OFF.SDR ASAA2023072144172Unknown · unknownFOUND LATCH FAULT BLEED FAMV RVDT L. GROUNDED - YES. C/W FIM FAULT ISOLATIONREF FIM 36-12-00-810-803, STEP A, B FAULT CLEAREDNO OTHER DEFECT NOTED.SDR ASAA2023072144163Unknown · unknownENG 2 DRIVE LIGHT NOT ILLUMINATED. GROUNDED - YES. PERFORMED #2 IDG OPS CHECK IAW AMM 24-11-00 OPS CK GOOD SEAMC DAVE NOTIFIED. NON ASA EMP KYLE WALEN A&P N9VR0841.SDR ASAA2023072144162Unknown · unknownDURING DESCENT, WITH MASTER CAUTION RECALL, SPEED TRIM FAIL ILLUMINATED. GROUNDED - YES. FCC "A" LOGGED 22-11186 FAULT. "B" SHOWS NO FAULTS LOGGED. PERFORMED IFIM 22-11-00-810-C61 & DETERMINED FAULT WAS A SOFTWARE NUISANCE FAULT. PERFORMED LRU TESTS SPEED TRIMSDR ASAA2023072144160Unknown · unknownCAPTAIN'S F/D MA GREEN LIGHT FLICKERS. GROUNDED - YES. (RESOLVED ON W/O: 1962645 TASKCARD: N/R-00001 ) PERFORMED LLM TEST AMM 22-11-00-700-801, ALL TEST PASSED, CLEARS MEL 22-11-12A & MEL 22-99B, PLACARD REMOVED, SEAMC PETER NOTIFIED.SDR ASAA2023072144159Unknown · unknownREF TC 05-020-01 - ENG #2 SMT ENG 2 EEC C1 SHORT TERM FAULT. GROUNDED - YES. NOTED NO CORRELATED FAULTS, ERASED LATCHED SMT MESSAGE. C/W TEST #32 - ENG IDLE SYSTEM TEST. ENG #2 SMT ENG 2 EEC C1 NO LONGER EXISTS. REF IFIM TASK G73-20-00-810-856.SDR DALA2023072405950Unknown · unknown(LOG 2877167) DURING HCK DENT LOCATED ON FORWARD CARGO COMPARTMENT LH SIDE BS 500C FRAME BETWEEN STRINGERS 25L AND STRINGER 26L. REMOVED DENT DAMAGE ON FORWARD CARGO COMPARTMENT LH SIDE BS 500C FRAME BETWEEN STRINGERS 25L AND STRINGER 26L IAW B737 SRM 53-30-07SDR ASAA2023072044177Unknown · unknownCA NAV DISPLAY SHOWED VTK WITH DUAL FMC FAILURE. BOTH FMC'S RECOVERED & VTK FLAG REEMOVED AFTER 30 SEC WITHOUT INTERVENTION. GROUNDED - YES. REBOOTED LT FMC - SYS OPS OK.SDR ASAA2023072044171Unknown · unknownWHILE PERFORMING TASK CARD 31-005-00 SCHEDULED MAINT TASK DISPLAY SYSTEM FOUND SMT MESSAGE BLEED CTRL CARD R. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072044141Modulating Valve · faultyREF T/C 31-005-00SMT "BLEED FAMV RVDT L" MESSAGE SHOWS WITH CORROLATED MAINTENANCE MESSAGE 36-12030 "ENG 1 FAMV RVDT SIGNAL IS OUT OF RANGE". GROUNDED - YES. (RESOLVED ON W/O: 1961274 TASKCARD: N/R-00001 ) REMOVED AND REPLACED FAMV ON #1 ENG. PERFORMED ELECTRISDR ASAA2023072044139Unknown · unknownREF. TC. 31-005-00 ENGINE NUMBER 1 SHOWS ACTIVE LATCHED FAULT CODE. 361-452-41. THE BLEED FAMV RVDT L. THIS SIGNAL IS OUT OF RANGE #36-12030. GROUNDED - YES. ON DEFERRAL.SDR DALA2023072405954Unknown · unknown(LOG 4404987) 3R DOOR EMERGENCY LIGHTS COME ON INTERMITTTENTLY INFLIGHT AND CAUSE EMERGENCY LIGHT TO ILLUMINATE ON CEILING ABOVE R REAR LAV. FOUND PIN 3 OF CONNECTOR D10744 PUSH BACK REINSERTED PIN PER B737 SWPM 20- 10. ALL CHKS GOOD.SDR ASAA2023072044138Unknown · unknownFMC DISAGREE ON SCRATCHPAD. GROUNDED - YES. ACCOMPLISHED IFIM 34-61-00-810-918. OPS NORMAL.SDR ASAA2023072044137Unknown · unknownHOT BATTERY CIRCUIT BREAKER POPPED. GROUNDED - YES. REF. AMM 20-60-01: ACCOMPLISHED INSPECTION AND SUBSEQUENT RESET OF P6-4 E15 (C134) CB OBSERVING NO DEFECTS. CONFIRMED CORRECT INDICATION RESTORED TO P5-13 DISPLAY W/ NO FAILURES SET. REF. AMM 24-21-53, WDM 24SDR ASAA2023072044136Unknown · unknownAPU GEN CONT UNIT CIRCUIT BREAKER OUT. GROUNDED - YES. RESET APU GEN CONT C/B ON P6-4 WITH NO FAULTS PER WDM 24-22-31-1 AND AMM 20-60-01. PERFORMED GOOD OPS TEST OF APU GEN PER AMM 24-21-00-700-801. NO HISTORY PAST 30 DAYS.SDR ASAA2023071944118Unknown · unknownPRESSURIZATION "AUTO FAIL" LIGHT CAME ON AT FL340 CABIN DIFT-7.8 CABIN PRESS 6500FT QRH 2.2 ACCOMPLISHED. GROUNDED - YES. ON DEFERRAL.SDR DALA2023072405949Unknown · unknown(LOG 2873763) MAIN PAX.CABIN,AFT.WET AREA FLOOR WEB HAS CORROSION,AT RBL.24 AND BS.1031. FABRICATED AND INSTALLED NEW MAIN PASSENGER CABIN AFT WET AREA FLOOR WEB AT RBL.24 AND BS1031 IAW BOEING DWG 147A5116-28 REV A, B737 SRM 51-40-05, B737 SRM 51-40-02 AND B7SDR DALA2023072405945Unknown · unknown(LOG 2874425) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR IB BALANCE BAY PANEL. REPAIRED CORRODED AREA PER DELTA ERA 609520-14.SDR DALA2023072405944Unknown · unknown(LOG 2874400) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR CENTER BALANCE BAY PANEL AT OB CORNER. REPAIRED CORRODED AREA PER ERA 609520-14 REV ORIGINAL.SDR DALA2023072405942Unknown · unknown(LOG 2874325) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR OB BALANCE BAY PANEL. REPAIRED AREA OF CORROSION PER ERA 609520-14 REV ORIGINAL.SDR DALA2023072405940Unknown · unknown(LOG 2874287) LH HORIZONTAL STABILIZER OB TE WEDGE UPPER ATTACH ANGLE HAS AREA OF CORROSION 28 FROM OB STABILIZER TIP. REPAIRED CORRODED AREA PER ERA 609520-14 REV ORIGINAL.SDR DALA2023072405939Unknown · unknown(LOG 2874072) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN STA 679 TO STA 706 BETWEEN S1 AND S-2R. C/W ER/A 610200-14 REV ORIGINAL.SDR DALA2023072405938Unknown · unknown(LOG 2874064) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN STA 730 TO STA 727B BETWEEN S1 AND S-2R. C/W ER/A 610223-14 REV ORIGINAL.SDR ASAA2023071844120Unknown · unknownUNABLE TO TRANSIT ON HF#1, HOWEVER,ABLE TO RECEIVE ON HF#1.HF#2 OPERATING NORMALLY. GROUNDED - YES. ON DEFERRAL.SDR DALA2023072405937Unknown · unknown(LOG 2872786) DURING INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE EXTERNAL SURFACE OF THE FUSELAGE CROWN UPPER SKIN BETWEEN APPROX. BS 678 AND BS 702, STR S-1 AND S-2R. REPAIRED CORROSION PER ERA 610200-14.SDR DALA2023072405935Unknown · unknown(LOG 2872766) DURING INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE EXTERNAL SURFACE OF THE FUSELAGE CROWN UPPER SKIN (PN 146A3101-38), BETWEEN APPROX. BS 727+16 AND BS 727A+17, STR S-1 AND S-2R. REPAIRED CORROSION PER ERA 610223-14.SDR DALA2023072405934Unknown · unknown(LOG 2872350) DURING INSTALLATION OF THE STRUCTURAL PROVISIONS FOR THE VIASAT RADOME PER AA 4430-01008-01D, SAL REPORTED THAT THEY HAD MISLOCATED A DOUBLER AT FITTING #2 RESULTING IN FASTENERS INSTALLED THROUGH THE CHEM-MILL LINE JUST INBOARD OF S-2R. HOWEVER,SDR ASAA2023071744110Unknown · unknownL FMC FAIL. GROUNDED - YES. ON DEFERRAL.SDR DALA2023072005881Unknown · unknown(LOG 2870942) TAIL STRIKE DAMAGE TO LOWER FUSELAGE SKIN BETWEEN STA 844. COMPLIED WITH ER/A 610419-14 REV. ORIG. ALL PRI 610419-14 REVS. 0 THRU 4 ARE COMPLIED WITH AND MATCH FINALE ER/A 610419-14 REV. ORIG.SDR DALA2023072005879Unknown · unknown(LOG 4833910) TAIL STRIKE ON LANDING DURING A BOUNCED LANDING PITCH ATTITUDE. BELLY SKIN DAMAGE BETWEEN STATIONS 847-887. REPAIRED ON NR 2 PER ERA 610419-14 REV ORG. TAIL SKID SHOE REPLACED ON NR 4, REF LOG 4833920. TAIL SKID CARTRIDGE REPLACED ON NR 5, REF LOSDR DALA2023072005878Unknown · unknown(LOG 2871014) CORROSION ON EXTERIOR FUSELAGE SKIN BETWEEN STA727 AND 727C, STR 2R AND 2L. C/W ER/A 610021-14 REV ORIGINAL.SDR ASAA2023071744085Unknown · unknownTECH SERVICES FOLLOW UP ON URGENT CNR 20230717011 FOR #1 ENG (60A677) CUMULATIVE ODMS CHIP COUNT INCREASE - LOW THRESHOLD **WITHIN NEXT 5 CYCLES**#PRI1/ETOPS. GROUNDED - YES. (RESOLVED ON W/O: 1962223 TASKCARD: N/R-00001 ) ACCOMPLISHED STEP 1 OF TSR , INSPECTISDR ASAA2023071744082Unknown · unknownWHEN PREFORMING TASK CARD 31-005-00 FOUND SMT MESSAGE ENG 1 EEC C2. GROUNDED - YES. THROUBLESHOT PER IFIM TASK G73-10-00-810-803 NO CORRELATED MAINTENANCE MESSAGES FOR ENG 1 EEC C2 SMT MESSAGE PER IFIM ERASED SMT MESSAGE AND PREFORMED ENG 1 IDLE SYSTEM TEST, T
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