Boeing 737-322
Service difficulty reports · 4,751
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 = '737322' 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 = '737322' 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 2005UALA00748Frame · gougedAFT CARGO DOOR LOWER AFT FRAME HAS .035 GOUGE WITH 15" LONG CRACK. REMOVED LOWER AFT FRAME. REMOVED INNER SUPPORT ANGLE. REINSTALLED ANGLE AND NEW FRAME. REF SRM 51-40-02. FRAME PN 65-47952-136.SDR 2005UALA00769Light · unknownMACH TRIM FAIL LIGHT ON RECALL, VERY CHRONIC. AFTER TROUBLESHOOTING & PARTS REPLACEMENT, REVIEW OF BITE DATA REVEALED INTERMITTENT MOMENTARY LOSS OF POWER TO MACH TRIM SYS. CIRCUIT BREAKER C1064, B-MACH TRIM DC, REPLACED & TEST FLT PERFORMED. INTERMITTENT NASDR 2005UALA00719Skin · crackedAPPROXIMATE 1.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R. REPAIRED DOOR 1R LOWER AFT CORNER REF SRM 53-10-01 PAGE 207.SDR 2005UALA00710Wire · inoperativeALL EEL LIGHTS AFT OF ROW 12 INOPERATIVE. REPAIRED POWER CABLE AND FEEDER CABLE.SDR 2005UALA00707Odor · detectedFLIGHT DIVERTED DUE TO ODOR IN CABIN. TOOK OFF AND RETURNED A SECOND TIME WITH SAME ODOR.SDR 2005UALA00704Wire · damagedEMERGENCY EXIT PATH LIGHTS STRIP INOP FROM ROW NR 15 AFT. REPLACED CABLE.SDR 2005UALA00703Guide Arm · damagedDOOR 2L EXTERIOR DOOR HANDLE RAISES IN SLIPSTREAM AND PARTIALLY ROTATES NO SPRING IN DOOR HANDLE, HANDLE HAS NO RESISTANCE WHEN PULLING OUT OR PUTTING BACK. SECURED EXTERNAL HANDLE, REPLACED GUIDE ARM, ADJUSTED STOP PIN.SDR 2005UALA00645Battery Pack · dischargedEXTERIOR EMERGENCY LIGHT NEXT TO DOOR 1R WON`T ILLUMINATE. BATTERY PACK NOT HOLDING CHARGE. REPLACED OK.SDR 2005UALA00616Battery Pack · dischargedEEL LIGHT INOP FROM ROW 17ABC THROUGH AFT GALLEY. LOW BATTERY REPLACED, OK.SDR 2005UALA00615Battery Pack · dischargedRIGHT OVERWING EMERGENCY EXIT SIGN AND SIDEWALL EXIT LIGHT INOP. LOW BATTERY REPLACED, OK.SDR 2005UALA00611Frame · chafedSTA 211 FRAME WEB WAS CHAFED BEYOND LIMITS BETWEEN STR 15R AND 16R, FRAME WAS ALSO GOUGED BEYOND LIMITS. SPLICED IN NEW SECTION OF WEB REF SRM 51-70-13 FIG 1 AND SPLICED IN NEW FRAME FROM STR 15R TO 17R REF SRM 51-70-12.SDR 2005UALA00603Cable · damagedEMERGENCY EEL LIGHTS INOP FROM ROW 17 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. SUPPLEMENTAL DATA UPDATE EEL CABLE WAS DAMAGED, REPLACED CABLE.SDR 2005UALA00598Attach Angle · crackedHORIZONTAL STAB CENTER SECTION CENTER LT SIDE 3 EACH BEAM ATTACHED ANGLES CRACKED, NR 1 UPPER FWD, NR 2 LOWER FWD AND NR3 LOWER AFT. REPLACED 3 EACH CRACKED FITTINGS REF SRM 51-40-02.SDR 2005UALA00586Bear Strap · crackedAFT CARGO DOOR CUTOUT AFT SIDE HAS BEAR STRAP REPAIR THAT WAS REMOVED WHEN ACCOMPLISHED SKIN REPLACEMENT. INSTALLED DOUBLER-TRIPLER REPAIR PER SRM 53-00-01 FIG 230.SDR 2005UALA00583Skin · dentedLT LEADING EDGE OF HORIZONTAL STABILIZER HAS DENT MIDWAY ON THE LEADING EDGE. CUTOUT DAMAGE & EVALUATED PER SRM 55-10-01. ACP NDT PER B737 NDT MANUAL NO DEFECTS NOTED. FABRICATED & INSTALLED INTERNAL DOUBLER REPAIR, FILLER & NEW RIB PER AAR EA I050118.SDR 2005UALA00581Wire · damagedEEL FLOOR LIGHTS ARE INOP FROM SEAT 16ABC TO AFT GALLEY. REPLACED EEL CABLE, OK.SDR 2005UALA00580Skin · damagedDURING FUSELAGE SKIN REPLACEMENT IN AFT PIT RT AFT LOWER FUSELAGE BS 800 RBL 25 STRINGER 25, SKIN HAS MISDRILLED HOLE. TRIPLER - FREEZE PLUG REPAIR ACP'D ON FWD LOWER CUTOUT PER SRM 53-00-01.SDR 2005UALA00579Lamp · damagedEEL LIGHTS AFT OF ROW 12 DO NOT LIGHT. REPLACED EEL LAMP, OK.SDR 2005UALA00575Lamp · damagedEEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CONTAINER STOWAGE. *S/D* REPLACED EEL LAMP, OK.SDR 2005UALA00574Wire · damagedEEL FLOOR LIGHTS INOP ROW 1-2AB. EEL CABLE REPLACED, OK.SDR 2005UALA00570Skin · gougedEXTERNAL FUSELAGE SKIN BELOW AFT PIT DOOR THRESHOLD SKIN HAS DEEP GOUGES. REMOVED DAMAGE, INSTALLED DOUBLER, TRIPLER AND QUADRUPLER PER EAI050117 AND BOEING 8100-9.SDR 2005UALA00566Pin · brokenTHE SAFETY PIN WAS BROKEN OFF IN THE CYLINDER HEAD. CAUSE COULD NOT BE DETERMINED. REMOVED THE BROKEN PIN FROM CYLINDER AND REPLACE WITH A NEW SAFETY PIN.SDR 2005UALA00563Door Frame · crackedFWD GALLEY DOOR AFT LWR FRAME CRACKED AT FASTENER HOLE. REPAIR ACP'D AT HMV4 AAR - REPLACED AFT FRAME PER SRM 51-40-02 & 51-10-02, GNMM 5-0-4-11 & 5-0-7-1.SDR 2005UALA00562Frame · crackedFWD GALLEY DOOR FWD LOWER FRAME CRACKED AT FASTENER HOLE. *S/D* REPAIR ACP'D AT HMV4 AAR WITH FWD FRAME REPLACEMENTT PER SRM 051-40-02 & 51-10-02, GNMM 5-0-4- -11 & 5-0-7-001.SDR 2005UALA00554Skin · dentedAFT CARGO DOOR EXTERNAL SKIN HAS SEVERAL DENTS BEYOND LIMITS. *S/D* REPAIR ACP'D AT HMV4 AT AAR-IND. ALL DAMAGES CUTOUT AND INSTALLED 43 X 48 INCH REPAIR DOUBLER PER SRM 52-30-01 FIG 202.SDR 2005UALA00553Frame · crackedRIGHT OVERWING FRAME INNER CHORD CRACKED THROUGH LOWER FASTENER HOLE AT BS 616 MID CABIN AREA. *S/D* REMOVED CRACK, FABRICATED STIFFENER ANGLE & FILLER AND INSTALLED REPAIR PER AMM 53-11-89.SDR 2005UALA00537Intercostal · wornDOOR 1L CUTOUT FWD FRAME HORIZONTAL INTERCOSTAL WORN AREA UPPER SURFACE JUST FWD OF LWR HINGE COVER. FABRICATED & REPLACE INTERCOSTAL PER SRM 53-10-15.SDR 2005UALA00531Light · inoperativeFLOOR MOUNTED EEL LIGHTS INOP FROM ROW 14 TO AFT GALLEY. POWER STRIP IN FLOOR TRACK WAS REPLACED.OKSDR 2005UALA00514Fire Loop · damagedFLIGHT DIVERTED TO DTW WITH A NR 1 ENGINE FIRE WARNING INDICATION. CREW REPORTED AT ROTATION OVERHEAT DETECTION LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW SHUTDOWN NR 1 ENGINE AFTER OVERHEAT LIGHT ILLUMINATED AGAIN AND DIVERTED THE AIRCRAFT TO DTW. FOUNSDR 2005UALA00550Rib · crackedLT HORIZONTAL STAB L/E RIB LOWER FLANGE AT STA 151.8 WAS FOUND CRACKED. *S/D* REPAIR ACP' D PER EVA-50305, FABRICATED REPAIR ANGLE REPAIR SCHEME AT HMV-4.SDR 2005UALA00549Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED AT AFT EDGE OF EQ COOLING EXHAUST OUTLET BS 378 LBL 02. *S/D* DURING REPAIR DETAILED IN MM53-30-99 (DOUBLER INSTALLATION), THE EXISITNG INTERNAL DOUBLER AROUND PERIMETER OF THE CUTOUT WAS TORN ADJACENT TO THE SKIN CRACK. THIS SDR 2005UALA00487Skin · dentedFWD CARGO DOOR HAS SEVERAL DENTS ON EXTERIOR SKIN. REPAIRED PER SRM52-30-01, LARGE 20 X 40 INCH DOUBLER INSTALLED ON OUTER EXT SKIN AT HMV-4.SDR 2005UALA00548Door Frame · crackedFWD GALLEY DOOR 2 EACH CRACKS FOUND AFT FRAME, FIRST CRACK AFT FRAME CUTOUT OF THE 3RD STOP, SECOND CRACK AROUND THE FASTENER HOLE ADJACENT TO THE LWR STOP. *S/D* FABRICATED AND INSTALLED DOUBLER PER CMM SM90-52-40-14JD AND BOEING REPAIR KIT 69-69854 INSTALLSDR 2005UALA00547Frame · dentedEXTERNAL FUSELAGE HAS A DENT AT FRAME STA 807 STR 28L & STR 28R. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED NEW SHEAR TIE CLIP SUPPORT ANGLE PER SRM 51-40-02 AND SRM 53-00-07.SDR 2005UALA00546Door Frame · crackedAFT CARGO DOOR FWD BS 795 FRAME WAS FOUND CRACKED AT JOINT WITH LOWER FRAME SECTION. *S/D* REPAIR ACP' D PER AAR EA I050096. FRAME SECTION WAS REPLACED USING A NESTED U-CHANNEL REPAIR SCHEME, AT AAR HMV-4.SDR 2005UALA00486Frame · crackedCABIN OVERWING BS 616 LT SIDE FRAME WEB INNER CHORD IS CRACKED THROUGH FIRST FASTENER APPROX 7 INCHES BELOW FLOOR. REPAIRED WEB AT BS 616 LT PER MM 53-11-81 AND REPAIRED FRAME INNER CHORD PER MM 53-11-89. MANUFACTURED ANGLE AND WEB AND INSTALLED.SDR 2005UALA00480Skin · damagedRT AFT FUSELAGE SKIN REPLACEMENT NEEDS DOUBLER REMOVAL AND INSTALLATION AFTER AFT SKIN IS REPLACED. REMOVED THE DOUBLER, ACCOMPLISHED HFEC OF THE HOLES. FOUND NO CRACKS, FABRICATED AND INSTALLED STRUCTURAL FILLER, DOUBLER AND TRIPLER PER SRM 51-00-01.SDR 2005UALA00473Odor · detectedACRID ELECTRICAL SMELL IN COCKPIT. NOT NOTED IN CABIN AND NO VISIBLE SMOKE. ELECTICAL SMELL IN FLIGHT DECK COULD ONLY BE SIMULATED WHEN TURNING ON WINDOW HEAT. REPLACED WINDOW HEAT SWITCH MODULE 69-37346-310 (MR30009). UNIT MR30009-9 WAS SENT TO SHOP 147. SDR 2005UALA00471Stringer Clip · crackedAFT PIT STA 727A STR 25L STR CLIP TO FRAME HAS A GAP. REMOVED AND REPLACED STR CLIP REF SRM 51-40-02.SDR 2005UALA00470Stringer · corrodedAFT PIT STA787+2 TO 787+4 STR 25L UPPER FLANGE IS EXFOLIATED LBL24-24. FABRICATED AND INSTALLED PARTS PER SRM 53-00-03.SDR 2005UALA00467Skin · punctured3-4 INCH DIAMETER HOLE PUNCTURED IN FUSELAGE SKIN ON RIGHT SIDE OF AIRCRAFT 6 FEET AFT OF RADOME AND 12 INCHES ABOVE NLG DOOR CUTOUT. SKIN IS ALSO DENTED 2 INCHES ABOVE PUNCTURE. THIS IS A MAJOR REPAIR INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-01 FIG 211 DSDR 2005UALA00458Skin · dentedEXTERIOR FUSELAGE BELOW 1R BETWEEN FRAMES 277 AND 294 STR 22R AND 23R BELOW A REPAIR DENTED. REMOVED THE DAMAGE FABRICATED A DOUBLER AND TRIPLER PER SRM 53-00-01 AND INSTALLED THE REPAIR PER SRM 53-00-01.SDR 2005UALA00457Light · shortedEMERGENCY EXIT FLOOR LIGHTS BEYOND ROW 15 INOP. LIGHT STRIP SHORTED, REPLACED.SDR 2005UALA00452Wire · cutAFT EEL LIGHTS FROM ROW 17 AFT INOP. FEEDER CABLE CUT OR DAMAGED - REPLACED.SDR 2005UALA00450Bear Strap · damagedAFT CARGO DOOR CUTOUT BEAR STRAP HAS PRE-EXISTING CUTOUT FOR REPAIR. *S/D* MAJOR REPAIR. INSTALLED DOUBLER-TRIPLER REPAIR PER SRM 53-00-01 FIG 230.SDR 2005UALA00446Anti-Ice Valve · inoperativeDIVERTED DUE TO INOPERATIVE NR 1 ENGINE ANTI-ICE VALVE. NR 1 ENGINE COWLING ANTI ICE VALVE FAILED.REPLACED VALVE PER AMM 30-21-11. NO FURTHER INCIDENT REPORTED.SDR 2005UALA00445Skin · dentedFWD CARGO DOOR EXTERNAL SKIN HAS SEVERAL DENTS INSIDE THE AREA OF FWD EDGE. REMOVED DAMAGE AND INSTALLED DOUBLER REF SRM 52-30-01 AND SRM 52-00-01 DURING DOOR OVERHAUL DURING HMV4.SDR 2005UALA00535Frame · crackedSTA 188 STR 17R FRAME CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER MM 53-11-83.SDR 2005UALA00534Frame · crackedSTA 188 STR 17L FRAME CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE PER MM 53-11-83.SDR 2005UALA00543Stringer Clip · damagedAFT PIT STA 747 STR 23L & STR 22L ARE DAMAGED. REMOVED AND REPLACED STRINGER CLIPS.
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