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 ASAA2023030942300Motor · faultyLEFT AFT FUEL PUMP "LOW PRESSURE" ILLUMINATED.(INFO: W/ 5175 LBS REMAINING IN TANK). GROUNDED - YES. REMOVED AND REPLACED LEFT AFT FUEL PUMP IAW B737-9 AMM 28-22-41-000-801 AND 28-22-41-400-801.SDR DALA2023031301808Intercostal · cracked(LOG 2662940) DURING INSPECTION FOUND CRACK WEB - INTERCOSTAL LOCATED BTW STA 500I TO 500J AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED WEB-INTERCOSTAL LOCATED BTW STA 500I TO 500J AT LEVEL STR 26L AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40-02SDR DALA2023031301807Intercostal · corroded(LOG 2662949) DURING INSPECTION FOUND CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BS947.5 AT LEVEL LBL47 AT AFT GALLEY AREA. REPLACED INTERCOSTAL LOCATED BETWEEN BS947.5 TO BS967 AT LEVEL LBL 47 AT AFT GALLEY AREA AS PER B737-900ER SRM 51-10-02- 0G PARAGRAPHSDR DALA2023031301806Web · corroded(LOG 2662945) DURING INSPECTION FOUND CORROSION WEB LOCATED BS986.5 TO BS1006 AT LEVEL LBL24.5 AT AFT GALLEY AREA. REPLACED WEB LOCATED BETWEEN BS986.5 TO BS1006 LEVEL LBL24.5 TO LBL 45 AFT GALLEY AREA AS PER B737-900ER SRM 51-10-02-0G AND SRM 51-40-02-0G AND SDR DALA2023031301805Support Fitting · corroded(LOG 2662934) DURING INSPECTION FOUND SUPPORT LOCATED STA 500L AND BTW STR 25R TO STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE SUPPORT AND FASTENERS LOC STA 500L BTW STR 25R TO 26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40-02-0G AND DRAWING D143SDR DALA2023031301804Shield · corroded(LOG 2662907) DURING INSPECTION FOUND CORROSION INTERNAL STRUCTURE ZEE CHANEL SIDEPLATE LOC BTW BS 847 AND BS 867 RBL 25.2 AFT CARGO COMPARTMENT. REPLACED INTERNAL STRUCTURE SHIELD ASSY LOC BTW BS 847 AND BS 867 RBL 25.2 AFT CARGO COMPARTMENT AS PER B737-900ERSDR ASAA2023030942263Unknown · unknownFOUND EMERG LIGHT OVER ROW 23RH INOP. GROUNDED - YES. FOUND ELECTRICAL CONNECTOR DISCONNECTED IN CEILING PANEL. RE-ATTATCHED & OPS TEST GOOD. REF B737-9 AMM 33-51-03.SDR ASAA2023030842311Exciter · failedMAINT LIGHT ILLUMINATED ON TAXI IN. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE RIGHT IGNITION SYSTEM IGNITOR. REF AMM 74-21-02. NO FIX. REMOVED AND REPLACED RIGHT IGNITION SYSTEM EXCITER. (REF ASA LP 60003520)SDR ASAA2023030842293Exciter · failed#2 ENG FAILED TO START ON RT IGN, N2-33%. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE RIGHT IGNITION SYSTEM IGNITOR. REF B737-9 AMM 74-21-02. NO FIX. REMOVED AND REPLACED RIGHT IGNITION SYSTEM EXCITER. OPS CHECK GOOD. REF AMM 74-11-01.SDR DALA2023031301803Intercostal · cracked(LOG 2661475) DURING INSPECTION FOUND CRACK WEB - INTERCOSTAL LOCATED BTW STA 500C TO STA 500D AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL AND FASTENERS LOC. BTW BS 500C TO BS 500D AT LEVEL STR 26R AT FWD CARGO COMPARTMENT AS PER B737SDR DALA2023031301802Intercostal · corroded(LOG 2661458) DURING INSPECTION FOUND CORROSION WEB - INTERCOSTAL LOCATED BTW STA 500G TO STA 500H AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BETWEEN STA 500G TO STA 500H AT LEVEL STR 26R AT FWD CARGO COMPARTMENT SDR DALA2023031301800Plate · corroded(LOG 2661494) DURING INSPECTION FOUND CORROSION SUPPORT ZEE SIDEPLATE BTW BS 727C PLUS 19 INCHES AND BS 727I LBL 25.2 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE (1 E/A), SPLICE SIDEPLATE (1 E/A) AND FASTENERS LOC. BTW STA 727L TO STA 847 STR 26L AFT CARGO COMSDR DALA2023031301799Plate · corroded(LOG 2661491) DURING INSPECTION FOUND CORROSION SUPPORT ZEE SIDEPLATE BTW BS 727I PLUS 8.5 INCHES AND BS 807 LBL 25.2 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE (2 E/A), SPLICE SIDEPLATE (1 E/A) AND FASTENERS LOC. BTW STA 727 TO STA 727L STR 26L AFT CARGO COMSDR DALA2023031301798Gusset · cracked(LOG 2661353) DURING INSPECTION FOUND CRACK GUSSET LOCATED AT STA 500L AND STR 19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED AT STA 500L AND STR 19R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-72-11 DWG # 143A7902.SDR ASAA2023030842251Filter · cloggedAPU LUBE FILTER DPI EXTENDED. GROUNDED - YES. REMOVED AND REPLACED APU LUBE FILTER AND RESET FILTER HOUSING DPI PER B737-9 AMM 49-91-12.SDR ASAA2023030842250Filter · faultyCAUTION OVERHEAD LIGHT ILLUMINATED FOR "MAINT" AFTER LANDING. GROUNDED - YES. FOUND LATCHED FAULT BLEED FAMV L. ACCOMPLISHED B737-9 IFIM 36-12020 STEP A-STEP C(2). CHANGED FAMV FILTER PER B737-9 AMM 36-12-03-100-801. ACCOMPLISHED PNEUMATIC ENG. ON SYS. TEST PESDR ASAA2023030742249Unknown · unknownWXR FAIL ENROUTE. GROUNDED - YES. ACCOM RESET OF WXR RT AND PERFORMED WXR OPS TEST REF B737-9 AMM 34-41-00. WXR TEST NORMAL NO OTHER FAULTS NOTED.SDR ASAA2023030742233Electronic Unit · failedFOLLOWUP TO HISTORY OF APU SHUTDOWN WITH ECU FAILURE MESSAGE. GROUNDED - YES. REMOVED AND REPLACED APU ELEC. CONTROL UNIT REF B737-9 AMM 49-61-12-000-801 AND 49-61-12-400-801.SDR ASAA2023030742232Unknown · unknownON LANDING ROLL MASTER CAUTION OVERHEAD MAINT LIGHT ILLUMINATED. GROUNDED - YES. A/C STATUS SHOWED BLEED FAMV L. CORRELATED MX MSG 36-12020 ENG 1 FAMV IS NOT IN COMMANDED POSITION. PER B737-9 IFIM 36-12-00-810-801 INITIAL EVAL. NO OTHER RELATED FAULTS. PERFORMSDR ASAA2023030742229Unknown · unknownSPEED TRIM LIGHT ILLUMINATED ON RECALL CHECK DURING DESCENT. RAN QRH CHECK. FOUND SINGLE CHANNEL FAULT. GROUNDED - YES. FOLLOWED B737-9 IFIM 22-11-00-810-071. PERFORMED DFCS FAULT HISTORY FOR CHANNEL A & B. FOUND CH:A, STAB TRIM CUTOUT RELAY, STAB TRIM SW/MODUSDR ASAA2023030742228Unknown · unknownAUTOTHROTTLE ANNUNCIATOR LIGHTS ON CAPTAIN PANEL INOP. GROUNDED - YES. FOUND CB D1 AT P18-1 POPPED. ACCOMPLISHED CIRCUIT BREAKER RESET TASK PER B737-9 AMM 20-60-01-860-801. CLOSED CB D1 AT P18-1. ACCOMPLISHED AUTOFLIGHT STATUS ANNUNCIATOR WARNING LIGHTS TEST PSDR ASAA2023030642267Unknown · unknownENGINE 2 EEC C1 FAULT WITH CORRELATED FAULT CODE 73245152 'ELECTRONIC OVERSPEED THRUST CONTROL MALFUNCTION ACCOMODATION TEST FAILED (SINGLE CHANNEL.)'. GROUNDED - YES. PER B737-9 FIM G73-20-00-810-856 NO SCHEDULED MAINT TASKS SHOW/ #2 ENGINE CORRELATED MSG 732SDR ASAA2023030642209Charger · inoperativeOVERHEAD ELEC ANNUNCIATOR ILLUMINATED ON TAXI OUT. GROUNDED - YES. REF B737-9 IFIM 24-31-00-810-802 BITE SHOWS "AUX BATT CHGR INOP" REPLACED AUX CHARGER REF B737-9 AMM 24-31-31/401.SDR ASAA2023030542255Unknown · unknownDURING APU START AT GATE, AUTO-SHUTDOWN AND APU FAULT LIGHT ILLUMINATED. EXTINGUISHED AFTER 4 MINUTES. GROUNDED - YES. ATTEMPTED 2ND START- START SUCCESSFUL-PERFORMED APU BITE PROCEDURE IAW B737-9 AMM 49-61-00. NO EXISTING FAULTS. FAULT HISTORY CHECK- 49-61144SDR DALA2023030701669None · none(LOG 2656734) DURING INSPECTION FOUND CRACK ANGLE LOCATED STA 500L AT LEVEL STR 28R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED STA 500L AT LEVEL STR 28R FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40-02-0G AND DRAWING 143A7902.SDR DALA2023030701668Intercostal · cracked(LOG 2656865) DURING INSPECTION FOUND FWD CARGO COMPARTMENT FUS. STRUCTURE INTERCOSTAL HAS A CRACK AT RADIUS FWD END, BS.500A STR.26R. REMOVED FABRICATED NEW AND INSTALLED FWD CARGO INTERCOSTAL @ STA 500A STR 26 RIGHT IAW B737 SRM 51-40-02 AND 53-30-53-01.SDR DALA2023030701667None · none(LOG 2656854) DURING INSPECTION FOUND FWD CARGO COMPARTMENT FUS. STRUCTURE MAIN FRAME IS BENT, BS.500J BETWEEN STR. 23R AND STR.25R. TRIMMED OUT DAMAGE 5" X 2" AND REPAIRED STA 500 J FRAME IAW B737 SRM 53-30-07.SDR DALA2023030701666None · none(LOG 2656848) DURING INSPECTION FOUND FWD CARGO COMPARTMENT FUS. STRUCTURE MAIN FRAME IS BENT BS 500K BETWEEN STR 24R AND STR 25R. TRIMMED OUT DAMAGE 7" X 2" AND REPAIRED STA 500K FRAME IAW B737 SRM 53-30-07 REPAIR 2.SDR DALA2023030701665Intercostal · cracked(LOG 2656617) DURING INSPECTION FOUND CRACK WEB - INTERCOSTAL LOCATED BTW STA 500C TO 500D AT LEVEL STR 26L. REPLACED WEB -INTERCOSTAL AND INSTALL BRACKET (2E/A) LOCATED BTW STA 500C TO 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40SDR ASAA2023030542189Unknown · unknownPILOT REPORTS MAINT LIGHT ON. GROUNDED - YES. INTERROGATED OMF, FOUND MAINT MESSAGE 21-65151 FOR CONT CAB TRIM VALVE SIGNAL OUT OF RANGE OR NOT IN COMMANDED POSITION. PERFORMED OPS TEST PER B737-9 IFIM 21-61-00-810-840. MAINT MESSAGE CLEARED.SDR ASAA2023030442234Unknown · unknownAMBER MAINT LIGHT ILLUMINATED. GROUNDED - YES. MDS STATUS INDICATES APU OIL QTY WITH A CORRELATED MAINTENANCE MESSAGE WITHIN EXTENDED - FAULT HISTORY: 49-94304 - NON-ACTIVE. ERASED LATCHED MESSAGE. RESTARTED APU AND OBSERVED CORRECT OIL QTY DISCRETE. FAULT DOESDR ASAA2023030442180Sensor · faulty#1 ENGINE ENG ANTI ICE COWL VALVE LIGHT ILLUMINATED TWICE. TURNED OFF WENT OUT. TURNED ON CAME BACK. GROUNDED - YES. CHECKED OMF FOR ANY EXISTING FAULT AND FOUND NO RELATED MAINT MSG. ACCOMPLISHED B737-9 IFIM TASK 30-21-00-810-807 COWL ANTI-ICE VALVE TEST GOODSDR ASAA2023030442173Unknown · unknownON FMC 1 MENU PAGE, NO SAT DISPLAYED. PERFORMED SAT LOCKUP QRH AND PROBLEM REMAINS. FMC 2 MENU DISPLAYS SAT BOTH BEFORE AND AFTER SAT LOCKUP QRH WAS PERFORMED. GROUNDED - YES. C/B RESET FOR # 1 FMCS COMPT AND # 1 CDU P18-1 PNL REF B737-9 AMM 20-60-05 SAT PROMPSDR ASAA2023030342191Starter · noneCFM IS REPORTING #2 ENGINE ODMS CHIP COUNT INCREASE ON A SINGLE FLIGHT. GROUNDED - YES. PERF ODMS SENSOR INSP IAW B737-9 AMM 79-00-00. PARTICLES CANNOT BE VISUALLY IDENTIFIED, TO BE SENT TO LAB FOR IDENTIFICATION. ODMS BUILDUP IS NORMAL FUZZ LEVEL. PERF SCAVENSDR ASAA2023030342186Unknown · unknownRIGHT FMC FAILED IN FLIGHT RAN QRH. RIGHT FMC REMAINED INOP. GROUNDED - YES. PERFORMED FMC SYSTEM OPERATIONAL TEST PER B737-9 AMM 34-61-00. SYSTEM TEST OK NO FAULT NOTED AT THIS TIME.SDR ASAA2023030342178Valve · failedWING ANTI-ICE= R VALVE= ILLUMINATED WITH SWITCH ON- EXTINGUISHED WITH SWITCH OFF. VALVE FAILED TO OPEN. GROUNDED - YES. REMOVED AND REPLACED RH WING THERMAL ANTI-ICE VALVE REF B737-9 AMM 30-11-11.SDR ASAA2023030342177Unknown · unknownON DESCENT WITH WING ANTI-ICE ON, "R VALVE" LIGHT ILLUMINATED. WITH SWITCH IN THE OFF POSITION, LIGHT EXTINGUISHED. GROUNDED - YES. REF ASA DATA SUPPLEMENT, C/W B737-9 AMM 30-11-11-710-801. OPS TEST OF WING THERMAL ANTI-ICE VALVE. CYCLED MULTIPLE TIMES. ALL OSSDR ASAA2023030342174Unknown · unknownHFI AND HF2 COMMUNICATION UNINTELLIGABLE ON EVERY FREQUENCY IN OCEANIC AIRSPACE. COMMUNICATION ON THESE RADIOS WAS SUCCESSFUL DEPARTING HAWAII. NO DIFFICULTIES RECEIVING SELCAL, HOWEVER VOICE COMMUNICATION WAS DIFFICULT. GROUNDED - YES. PERFORMED HF #1 & HF #2SDR ASAA2023030342172Unknown · unknownON INITIALLY SETTING POWER (AT APPROX 50%) "STAB OUT OF TRIM" LIGHT ILLUM. (LOW SPEED <10 KTS). WE ABORTED AND DID A CONFIG CHECK - WE RECEIVED A TAKEOFF WARNING. ONCE CLEAR, LT EXTINGUISHED. GROUNDED - YES. DFCS BITE B737-9 DFCS FIM TASK 22-11-00-810-D72.SHOWSDR DALA2023030601629None · none(LOG 8779501) DURING INSPECTION FOUND FUSELAGE DAMAGE LEFT HAND AT STA 500, 500A AND STRINGERS S-21L, S-22L. REPAIRED FUSELAGE DAMAGE PER DETA ERA 600864-14 REV 0.SDR ASAA2023030242187Unknown · unknownWING ANTI-ICE R VALVE ILLUMINATED WHEN USING SYSTEM INFO DUCT SPLIT 25PSI+ WHEN USING. GROUNDED - YES. PERFORMED B737-9 IFIM TASK 30-11-00-810-809 A.1,A,B,C, AND E. MANUAL OVERRIDE MOVES FREELY. FOUND BOTH WING ANTI ICE LTS OFF AND HAD CREW RUN ENGINES AT IDLESDR ASAA2023030242176Unknown · unknownWING ANTI-ICE R VALVE ILLUMINATED TURNING ON WING ANTI ICE MASTER CAUTION-ANT ICE A FEW SECONDS LATER. LIGHT WENT OUT AFTER TURNING WAI OFF. CYCLED SWITCH AGAIN SAME RESULT LEVEL AT 5000FT 210 KTS. GROUNDED - YES. PERFORMED WING THERMAL ANTI ICE VALVE OPERATIOSDR DALA2023030601628Tie Clip · cracked(LOG 2652403) DURING INSPECTION FOUND CRACK TIE CLIP LOCATED STA 500L AND STR 26R AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED STA 500L AND STR 26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-10-02 ITEM 9 AND DWG 143A1262.SDR DALA2023030601627Angle · cracked(LOG 2652394) DURING INSPECTION FOUND CRACK ANGLE - CLIP LOCATED AFT FACE OF THE STA 500K AND STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP LOCATED AFT FACE OF THE STA 500K AND STR 26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-10-02 ITEM 9ANDSDR DALA2023030601626Angle · cracked(LOG 2652386) DURING INSPECTION FOUND CRACK ANGLE LOCATED AFT FACE OF THE FRAME STA 500I AND STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED AFT FACE OF THE FRAME STA 500I AND STR 26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-10-02 ITEM 9AND DSDR DALA2023030601625None · none(LOG 2652382) DURING INSPECTION FOUND CRACK ANGLE LOCATED STA 500K AND STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED STA 500K AND STR 26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-10-02 ITEM 9 AND DWG 143A7505.SDR DALA2023030601624None · none(LOG 2652377) DURING INSPECTION FOUND CRACK ANGLE LOCATED AFT FACE OF THE STA 500J AND STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED AFT FACE OF THE STA 500J AND STR 26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-10-02 ITEM 9 AND DWG 143A7505SDR DALA2023052204089Unknown · unknown(LOG 2650930) DURING ACCOMPLISHMENT OF AIRCRAFT 3953, IT WAS FOUND THAT THE CURRENT DESIGN OF THE RETAINER PLATE DOES NOT ALLOW THE QUARTER TURN RETAINERS ON THE LEFT-HAND SIDE OF COMPARTMENT 414 IN GALLEY G4C TO TURN CORRECTLY AND THAT THERE IS AN OVERHANG OFSDR DALA2023052204088Unknown · unknown(LOG 2650925) DURING ACCOMPLISHMENT OF AIRCRAFT 3953, IT WAS FOUND THAT THE CURRENT DESIGN OF THE RETAINER PLATE DOES NOT ALLOW THE QUARTER TURN RETAINERS ON THE LEFT-HAND SIDE OF COMPARTMENT 414 IN GALLEY G4C TO TURN CORRECTLY AND THAT THERE IS AN OVERHANG OFSDR ASAA2023030142353Sensor · out of rangeDURING ASA TC 05-020-01 FOUND REPEAT ENG 2 EEC C2 FAULT. 77-43073, N2 SENSOR OUT OF RANGE. GROUNDED - YES. REMOVED AND REPLACED ENG #2 N2 SPEED SENSOR PER B737-9 AMM 77-12-02.
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