Boeing 737-2Y5
Service difficulty reports · 334
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 = '7372Y5' 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 = '7372Y5' 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 SPA2008F00002Battery Pack · inoperativeLOWER EMERGENCY EXIT LIGHT AT R1 AND L1 DOOR POSITIONS WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MANUAL 33-21-27. FUNCTIONAL CHECK SATISFACTORY. (K)SDR SPA2008F00001Battery Pack · inoperativeLOWER EMERGENCY LIGHTS AT DOORS L2 AND R2 WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-21-27. FUNCTIONAL CHECK SATISFACTORY. (K)SDR SPA2008F00000Battery Pack · failedMID CABIN CEILING EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK AND POWER SUPPLY IAW MM 33-51-81. FUNCTIONAL CHECK SATISFACTORY. (K)SDR SPAA0800096Power Supply · inoperativeAFT SECTION OF FLOOR PATH ESCAPE LIGHTING INOPERATIVE. REPLACED FLOOR TRACK POWER SUPPLY IAW MM 33-21-27. OPS CHECK SATISFACTORY.SDR TSAA0732043Module · failedNON-ETOPS FLIGHT 221 OGG - HNL. WHEN THE CREW SELECTED THE LANDING GEAR TO UP, THE LT MAIN GEAR DOWN LIGHT TOOK A FEW SECONDS LONGER TO EXTINGUISH THAN THE OTHER GEAR INDICATIONS. AFTER THE GEAR LEVER WAS SELECTED TO OFF, THE LT MAIN GEAR EXTENDED UNCOMMANDESDR TSAA0729040Hose · failedFLIGHT 26 HNL-OGG - AFTER TAKEOFF FROM HNL, CREW NOTED LOSS OF SYSTEM A HYDRAULIC PRESSURE. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE TOWED THE AIRCRAFT TO THE GATE AND REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR HYDRAULIC SURGE RELIEF LSDR TSAA0726029Fire Detector · failedFLIGHT 93 HNL-LIH - AFTER STARTING THE NR 1 ENGINE, THE CREW NOTED THE NR 1 ENGINE FIRE INDICATION LIGHT ILLUMINATED. CREW FOLLOWED THE QRH PROCEDURES: SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AIRCRAFT WAS TOWED BACK TO THESDR SPAA0700090Battery Pack · inoperativeMID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT POWER SUPPLY (BATTERY PACK) PER AMM 33-51-111, OPS CHECK SATISFACTORY.SDR TSAA0632057Wheel · separatedON LANDING, CREW HEARD AN UNUSUAL (BUMP) NOISE WITH NORMAL LANDING. TAXI TO GATE WITHOUT FURTHER INCIDENT. CREW FOUND NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY HAD SEPARATED FROM THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MLG BRAKE ASSEMBLY AND THESDR SPAA0600087Battery Pack · dischargedLEFT OVERWING EXIT LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AND TESTED SERVICEABLE IAW 33-51-11, OPS CHECK NORMAL.SDR SPAA0600086Battery Pack · dischargedLEFT OVERWING EXIT LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AND TESTED SERVICEABLE IAW 33-51-11, OPS CHECK NORMAL.SDR SPAA0600084Battery Pack · dischargedLEFT OVERWING EXIT LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AND TESTED SERVICEABLE IAW 33-51-11, OPS CHECK NORMAL.SDR SPAA0600088Battery Pack · dischargedLEFT OVERWING EXIT LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AND TESTED SERVICEABLE IAW 33-51-11, OPS CHECK NORMAL.SDR SPAA0600085Battery Pack · dischargedLEFT OVERWING EXIT LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AND TESTED SERVICEABLE IAW 33-51-11, OPS CHECK NORMAL.SDR TSAA0651040Spar · corrodedHORIZONTAL STABILIZER RT REAR SPAR UPPER CHORD CORROSION (3 AREAS).SDR TSAA0651039Spar · corrodedVERTICAL STABILIZER RIGHT T/E REAR SPAR CORROSION (3 AREAS).SDR TSAA0653018Skin Panel · crackedA 2 INCH SKIN CRACK AT BS 929 STR 24L. A .04 INSURANCE MADE IAW SRM 53-30-3. RIVET PATTERN LAID OUT AND DRILLED AND MANUFACTURED REPAIR DOUBLER, TRIPLER, AND 2 FILLERS PER SRM 53-30-3 FIG 48 DET XIX. HFEC RIVET HOLES IAW BOEING NDT MANUAL 51-00-00 PT 6. RESDR SPAA0600083Power Supply · dischargedDURING ACCOMPLISHMENT OF A CHECK, LEFT OVERWING AND LOWER AFT EMERGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED AFT CARGO COMPARTMENT EMERGENCY EXIT POWER SUPPLY AND BATTERY PACK PER AMM 33-51-31. OPERATRIONAL CHECK SATISFACTORY.SDR TSAA0653017Spar · corrodedCORROSION ON UPPER & LOWER SURFACE OF FRONT SPAR LOWER CORD BETWEEN FSS 297 & FSS-306 AT SLAT NR 4. BLENDED INBOARD - OUTBOARD DIRECTION 10:1 DEPTH TO BLEND RATION. SHOT/FLAP PEEN BLENDED ARE PER SRM. FABRICATED SOLID FILLERS TO REPLACE REMOVED MATERIAL. FSDR TSAA0621007Fan · defectiveON APPROACH THE PILOT SMELLED SMOKE AND AFTER LANDING THE SMELL GREW STRONGER. AIRPLANE TAXIED BACK TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED GASPER FAN. OPS CHECK GOOD, NO HELP. THE CABIN AUGMENTATION FAN WAS FOUND TO BE INOP. REMOVED AND REPLACSDR TSAA0653006Skin · crackedA 4 INCH FUSELAGE SKIN CRACK BS 937 AT STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 24 X 20 INCH SKIN PATCH, FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER NR 5 AND 6 PER SRM 53-30-3, FIG 48, DET XII.SDR SPAA0500078Battery Pack · dischargedSCHEDULED MAINTENANCE VISIT, FWD DOOR AREA CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW B737MM 33-51-02. OPERATIONAL CHECK NORMAL.SDR SPAA0500048Battery Pack · dischargedSCHEDULED MAINTENANCE VISIT, FWD DOOR AREA CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW B737MM 33-51-02. OPERATIONAL CHECK NORMAL.SDR SPAA0500077Battery · dischargedEMERGENCY FLASHLIGHT BATTERY DEAD AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW MM 25-69-0 AND 20-50-11, OPS CHECK NORMAL.SDR SPAA0500047Battery · dischargedEMERGENCY FLASHLIGHT BATTERY DEAD AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW B737MM 25-69-0 & 20-50-11, OPS CHECK NORMAL.SDR TSAA0575031Bleed Valve · defectiveON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00. R.I.I. COMPLETED FOR NR 2 ENG PRBC VALVE CHANGE IAW MM 75-31-11. DID NOT FIX OFF IDLE STALL. LSDR TSAA0575029Bleed Valve · defectiveRUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 OPS CHECK OK ON NR 2 ENGINE. BLEED VALVE SCHEDULING COMPLETED PER PWA MM 72-00-00. LUBED 8TH ANSDR SPAA0400073Skin · corrodedCORROSION DAMAGE WAS FOUND ON THE LT UPPER WING SKIN P/N 65C17191-1 AT THE REAR SPAR AT APPROXIMATELY WS 442.0. THE CORROSION WAS REMOVED AND TRIMMED AND A REPAIR SCHEME WAS PROVIDED BY BOEING ENGINEERING. THE CORROSION AREA WAS REPAIRED PER BOEING INSTRUCTIONSDR SPAA0400070Battery Pack · inoperativeR2 DOOR EMERGENCY BATTERY PACK DOES NOT OPERATE. REPLACED R2 DOOR EMERGENCY BATTERY PACK IAW BMM 33-51-101, OPERATIONAL CHECK GOOD.SDR SPAA0400069Light · inoperativeON PREFLIGHT FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECK GOOD.SDR TSAA0479019Engine · leakingFLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AND SHUTDOWN THE NR 1 ENGINE. DECLARED EMERGENCY AND HAD UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 1 ENGINE PER FORMS M-211 THROUGH M-SDR SPAA0400068Pin · installedL-2 DOOR ESCAPE SLIDE DID NOT DEPLOY DURING CABIN CREW TRAINING EXERCISE. FOUND DISCHARGE BOTTLE SAFETY PIN INSTALLED. MAINTENANCE REMOVED SAFETY PIN, CREW TRAINING RESUMED, SLIDE DEPLOYED.SDR TSAA0429001Line · failedFLT 240 - HNL-OGG - ON GEAR RETRACTION 'A' SYSTEM HYDRAULIC ANNUNCIATOR LIGHT CAME ON. SYSTEM QUANTITY AT 1.5 GALLONS. RETURNED TO HNL. FOUND RIGHT MAIN GEAR UPLOCK ACTUATOR FLEX-LINE RUPTURED. REMOVED AND REPLACED FLEX-LINE. LEAK CHECK OK. SERVICED HYDRASDR SPAA0300067Battery Pack · intermittentON PREFLIGHT CHECK, NOTED MID CABIN CEILING EMERGENCY LIGHT SIGN FLICKERING. REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD.SDR TSAA0333205Battery Pack · inoperativeREPLACED AFT ENTRY DOOR IDENT EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR F3LA200300114Fitting · corrodedDURING C-4 CHECK, INSPECTION REPORTED RT. HORIZONTAL STAB CENTER SECTION, AFT UPPER ATTACH CLEVIS, AFT LUG, CORRODED. REPAIRED PER EA 55-737-077.SDR F3LA200300113Door Frame · corrodedDURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR FRAME ON FUSELAGE CORRODED ON AFT SEALING SURFACE BETWEEN BOTTOM TO SECOND FROM BOTTOM STOP PAD FITTINGS. BLENDED AREA AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PER SRM 53-30-03, FIG. 46 AND EA 53-737-199SDR F3LA200300094Panel · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SERVICE PANEL CORRODED AT FWD HINGE. FOUND TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED REPLACEMENT PANEL AND DOUBLER PER EA 52F-737-091. ALODINED PER SRM 51-21-41, PRIMED AND PAINTED PER SOPM 20-41-02.SDR F3LA200300092Web · corrodedDURING C-4 CHECK, INSPECTION REPORTED LOWER WEB FROM LAVATORY FLOOR TO FUSELAGE ON LT. SIDE OF FUSELAGE CORRODED AROUND CUTOUTS, STA. 277 TO STA. 294.5. FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-10-01, 51-40-02 AND SOPM 20-41-02.SDR F3LA200300091Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM AT STA. 772, LBL 12, AT FLOOR PANEL SPLICE STRIP, BOTTOM SIDE OF UPPER FLANGE. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-5 AND SOPM 20-41-02.SDR F3LA200300090Mount Bracket · crackedDURING C-4 CHECK, INSPECTION REPORTED FWD FUSELAGE VHF 2 ANTENNA MOUNT BRACKET CRACKED AT STA. 500, RBL 2. REPLACED BRACKET PER SRM 51-10-1 AND 51-30-2.SDR F3LA200300089Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR RT. MOP SILL CORRODED AT VARIOUS POINTS ALONG ENTIRE LENGTH OF MOP SILL. REPLACED DAMAGED MOP SILL PER SRM 51-30-2 AND BOEING DRAWING 65-45855.SDR F3LA200300088Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT/INTERCOSTAL (WEB STRAP)FROM STA. 1006 BACK, LBL 2, CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP AND GALLEY BRACKET FROM STA. 1006 TO STA. 1031, LBL 2, PER SRM 51-30-02 AND BOEING DRAWING 6SDR F3LA200300087Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FIG. 1, SHEET 4, DETAIL I. REPLACED SILL PER SRM 51-10-2 AND SRM 51-30-02.SDR F3LA200300086Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 927 AND STA. 947.5 ON RT. SIDE OF AIRCRAFT CENTERLINE CORRODED. REMOVED CORROSION AND INTERCOSTAL PER SRM 51-30-02. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-10-06. FABRICATED AND INSTALLEDSDR F3LA200300085Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT CARGO FLOOR SUPPORT CORRODED ON LOWER FLANGE AT STA. 859, RBL 8. INSTALLED REPAIR PER SRM 53-10-5 AND MM 51-21-99.SDR F3LA200300084Web · corrodedDURING C-4 CHECK, INSPECTION REPORTED WEB BETWEEN STA. 332 AND STA. 344, AFT OF R-1 DOOR, CORRODED ON BOTTOM SIDE. REMOVED DAMAGE ON WEB, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2, PAGES 1-3 AND SOPM 20-41-02.SDR F3LA200300083Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION IN SCREW HOLES OF FWD LAVATORY AFT BULKHEAD ATTACH ANGLE, HAT SECTION, STA. 312, LBL 12 TO LBL 42. REMOVED HAT SECTION PER SRM 51-30-2. FABRICATED AND INSTALLED NEW HAT SECTION PER SRM 51-10-1, SRM 51-30-2 AND SDR F3LA200300082Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED SHORT INTERCOSTAL AT CENTERLINE BETWEEN STA. 1006 AND STA. 1016 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SOPM 20-41-02.SDR F3LA200300081Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED LT. INTERCOSTAL BETWEEN STA. 967 AND STA. 986.5 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SOPM 20-41-02
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