Boeing 737-3S3
Service difficulty reports · 1,209
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 = '7373S3' 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 = '7373S3' 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 AWXA200200097Windshield · crackedGEG - DIVERSION - FLT 592 - O - EN ROUTE FROM GEG TO PHX AT FL 330 CABIN PRESSURE DIFFERENTIAL OF 7.8 PSI CAPTAINS WINDSHIELD OUTER PANE SHATTERED. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED SAFELY TO BOI. MAINTENANCE ARRIVED AT BOI FROM PHX AND REPLACED TSDR AWXA200200058Stiffener · corrodedMCN - MAJOR REPAIR - C - DURING INSPECTION MAINTENANCE FOUND CORROSION ON AFT PRESSURE BULKHEAD STIFFENERS AT BS 1016, BL 0. MAINTENANCE REMOVED CORROSION FROM AFT PRESSURE BULKHEAD STIFFENERS AT BS 1016 AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SECTIONSDR AWXA200200020Web · deformedMCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND EVIDENCE OF DEFORMED MATERIAL ON THE FWD CARGO DOOR INNER SKIN LIGHTING HOLES, 3RD ROW OF HOLES FROM BOTTOM AT FWD SIDE OF DOOR BS 440 TO BS 460. MAINTENANCE REMOVED DAMAGED PORTION OF WEB AT TWO POSDR AWXA200200037Crossbeam · crackedMCN - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON THE VERTICAL LEG OF THE FORWARD CARGO DOOR LOWER OUTER TEE CHORD AFT END BS 487. MAINTENANCE CUTOUT DAMAGED SECTION OF CRACKED TEE CHORD AT BS 487, TRIMMED NEW REPLACEMENT SECTION OF TEE CHORD, FSDR AWXA200200060Floorbeam · corrodedMCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED CORROSION ON MAIN CABIN FLOORBEAM AT PREVIOUS REPAIR FILLER, BS 967, LBL 28, WL 208.1. MAINTENANCE REMOVED REPAIR ANGLES AND FILLER AT BS 967 BEAM, CLEANED CORROSION ON FILLER AND FOUND MATERIASDR AWXA200200039Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-15 CHECK 1" CRACK IN FUSELAGE EXTERNAL SKIN WAS FOUND AT THE L1 DOOR LOWER AFT CORNER OF CUTOUT BS 339.5, CRACK CONFIRMED BY 10X VISUAL AND HFEC INSPECTION. MAINTENANCE STOP DRILLED CRACK AT L1 DOOR CUTOUT LOWER AFT CORNER BSDR AWXA200200018Floor Support · corrodedMCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED FLOORBOARD SUPPORT ANGLE CORRODED AT BS 947 TO BS 987, RBL 55, WL 208.1. MAINTENANCE REMOVED CORROSION FROM FLOORBOARD SUPPORT ANGLE AND PERFORMED MATERIAL THICKNESS MEASUREMENT WITH LOSS OF MASDR AWXA200200017Support · corrodedMCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED SUPPORT ANGLE CORRODED AT FASTENERS BS 995, LBL 46. MAINTENANCE REMOVED AND REPLACED CORRODED INNER CHORD AND SUPPORT ANGLE IAW B737-300 SRM 53-60-13 FIG 101 PG 104-107, 51-40-05 PG 1-2, 51-40-SDR AWXA200200011Floorbeam · corrodedMCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND CORRODED FLOORBEAM AT BS 967, FROM RBL 15 TO RBL 18, WL 208.1. MAINTENANCE CLEANED AND BLENDED CORRODED SECTION OF FLOORBEAM AND PERFORMED MATERIAL THICKNESS MEASUREMENT FINDING MATERIAL LOSS OUT OFSDR AWXA200200038Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND A 1 1/2" CRACK AT THE L2 DOOR FWD LOWER CUTOUT THAT EXTENDS OUT OF A COUNTER SUNK SCREW HOLE BS 960, CRACK WAS VERIFIED BY HFEC INSPECTION. MAINTENANCE CUTOUT CRACKED AREA OF OUTER SKIN AND FABRICASDR AWXA200200043Frame · crackedMCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE DISCOVERED CRACKED FRAME AT FASTENER BS 616, RBL 64. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME, HFEC INSPECTION COMPLIED WITH TO VERIFY CRACK CONTAINED, FABRICATED AND INSTALLED REPAIR STIFFENER ANGLE AND SDR AWXA200200016Frame · crackedMCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE DISCOVERED CRACKED FRAME AT FASTENER BS 616, LBL 64. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME, DAMAGED AREA WITHIN REPAIRABLE LIMITS IAW AWA ER 03-5311-01143-DD1. HFEC INSPECTION COMPLIED WITH TO VERIFY SDR AWXA200200012Skin · chafedMCN - MAJOR REPAIR - "C" - DURING C-15 CHECK MAINTENANCE FOUND FUSELAGE SKIN CHAFED BELOW R/H HORIZONTAL STABILIZER APPROXIMATELY 50" AFT OF STABILIZER LEADING EDGE BS 1133. MAINTENANCE BLENDED CHAFED AREA OF SKIN AND PERFORMED MATERIAL THICKNESS MEASUREMENT FSDR AWXA200200044Skin · bentMCN - MAJOR REPAIR - "C" - DURING C-15 CHECK THE UPPER AFT CORNER OF THE FORWARD GALLEY SERVICE DOOR WAS FOUND TO HAVE SKIN BENT OUTWARD. MAINTENANCE REMOVED DAMAGED SKIN AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIRS IAW B737-300 SRM 52-00-01,SDR AWXA200100610Wire · detachedYVR - EEL - "C" - DURING C-15 CHECK DISCOVERED BLACK WIRE PULLED OUT OF SPLICE IN FLOOR CONDUIT ON L/H SEAT MOUNTED ESCAPE PATH LIGHTING SEAT ROW 17. MAINTENANCE RE-SPLICED WIRE PER STANDARD WIRING PRACTICES MANUAL 20-30-12, PG. 3.SDR AWXA200100635Web · crackedPHX - MAJOR REPAIR - "C" - 1.5" CRACK FOUND ON RADIUS OF INTERCOASTAL AND STRAP AT FWD LAV ATTACH POINT BS 305, STR 5L. MAINTENANCE REMOVED CRACKED INTERCOASTAL AT BS 305 AND STRAP AT STR 5L: FABRICATED NEW INTERCOASTAL AND STRAP, AND INSTALLED REPAIR PARTS IASDR AWXA200100576Skin · crackedLAS - B3 CK - C - CRACK FOUND IN FUSELAGE SKIN 1.375 INCH LONG AT BS 727D, STR 23L. MAINTENANCE ROUTED OUT THE CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED IAW AWA ER 03-5331-01310-TB1.SDR AWXA0001851Pump · leakingAIR TURNBACK,EN ROUTE FROM LAS TO SNA THE A/C LOST B-HYD SYSTEM QUANTITY AND THE NR 2 ENG DRIVEN HYD PUMP LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY THE B-SYSTEM ELEC PUMP LOW PRESSURE LIGHT. A/C RETURNED TO LAS MAKING AN UNEVENTFUL LANDING. MX FOUND HYD FLUSDR AWXA0001611Connector · shortedPHX - AIR TURNBACK - 4/9/01 - ON CLIMBOUT NR 1 EGT GAUGE NEEDLE DROPPED TO 0; THE CREW RESET THE NR 1 EGT CIRCUIT BREAKER AND THE NEEDLE DROVE UP TO THE ASSUMED TEMP THEN DROPPED BACK DOWN. THE AIRCRAFT RETURNED TO PHX FOR REPAIR; THIS PROBLEM HAD SOME RECENTSDR AWXA0001607Floorbeam · crackedREMOVE BLOCK ON BOTTOM SIDE OF UPPER FWD LIP OF FLOORBEAM AT LBL 45.5 FOR FURTHER CRACK INSPECTION BS 520. INSPECTED AND REPAIRED CRACK IAW EO 53-14-12 REV C.SDR AWXA0001606Web · crackedFLOOR STRUCTURE AT WL 207 AFT SIDE OF FS 178 BLKHD HAS A CRACK EXTENDING O/B FWD SIDE CHORD. REMOVED AND REPLACED WEB ON AFT SIDE OF BLKHD WL 180 - 225, RBL 18 IAW SRM 51-40-02 PG 1.SDR AWXA0001585Pressure Panel · crackedCRACK IN LT WHEEL WELL PRESSURE PANEL AT FS 663 LBL 34. TRIMMED OUT DAMAGED AREA; FABBED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLER, STIFFENER AND CHANNEL IAW AWA ER 03-5710-01073-JS1.SDR AWXA0001583Rib · chafedRIB AND CHAFE STRIP WORN THROUGH ON I/B END OF LEFT O/B MID FLAP. REMOVED AND REPLACED RIB AND CHAFE STRIP IAW B737-300 SRM 51-40-02 PG 3 & 6 AND 51-40-05 PG 2.SDR AWXA0001584Frame · crackedFWD CARGO COMPARTMENT STA 500 FRAME HAS A .125 INCH CRACK AT RBL 5. FABBED REPAIR ANGLE AND FILLER; LOCATED, DRILLED AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 AND 51-70-11 FIG 1 PG 1 - 6.SDR AWXA0001582Attach Angle · damagedFS 178 BLKHD WL 195 RBL 24-28 ATTACH ANGLE HAS ELONGATED HOLES. REMOVED AND REPLACED ANGLE AND CLIP IAW BOEING DWG 65-16301 AND SRM 51-40-02 PG 10.SDR AWXA0001565Frame · damagedSTA 500 FRAME ELONGATED HOLES IN LOWER WEB BETWEEN STR 28R AND 28L. FABBED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND CLIPS IAW AWA ER 03-5332-01087-DD1.SDR AWXA0001564Floorbeam · crackedCABIN FLOOR SUPPORT UPPER T-ANGLE AND WEB CRACKED AT FS 663.75 BL 0. FABBED, DRILLED AND INSTALLED REPAIR WEB SPLICE PLATES AND ANGLES IAW AWA ER 5702-01074-JS5 AND B737-300 SRM 51-10-02 PG 15 AND 51-40-02 PG 10.SDR AWXA0001546Bulkhead · crackedFS 178 BLKHD CENTER WEB IS CRACKED AT 2 PLACES LBL 10.8 AND 11.7 WL 234.1. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001545Web · crackedFLOOR STRUCTURE AT WL 207 AFT SIDE OF FS 178 BLKHD HAS A CRACK EXTENDING O/B TOWARDS SIDE CHORD. REMOVED AND REPLACED WEB (WL 180 - 225 LBL 18 AND RBL 18) IAW SRM 51-40-02 PG 1.SDR AWXA0001544Bulkhead · crackedFS 178 BLKHD CENTER WEB IS CRACKED (2 CRACKS) AT LBL 1.5 WL 187.25-188 AND AT RBL 1.5 WL 187-188.25. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001543Bulkhead · crackedFS 178 BLKHD CENTER WEB IS CRACKED AT LBL 4.8 WL 198.4 AND WL 201.2 - 201.5. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001542Bulkhead · crackedFS 178 BLKHD CENTER WEB IS CRACKED AT LBL 7 WL 200.75 TO 201.25. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001541Bulkhead · crackedFS 178 BLKHD CENTER WEB IS CRACKED AT RBL 1.0 WL 205.5. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001540Bulkhead · crackedFS 178 BLKHD WEB IS CRACKED AT LBL 1.5 WL 205.8 BELOW T-ANGLE. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND STRAP IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001539Bulkhead · crackedFS 178 BLKHD WEB IS CRACKED AT RBL 4.8 WL 198.7 AND 199.3 AND 199.9. REMOVED FASTENERS; CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-10-08 PG 1-11 FIG 211.SDR AWXA0001538Frame · crackedFS 178 BLKHD WEB VERTICAL CHORD IS CRACKED AT LBL 5.7 WL 173 - 174.5. REPAIRED VERT CHORD IAW SRM 53-10-08 PG 221-252 FIG 205.SDR AWXA0001517Intercostal · damagedINTERCOSTAL ADJACENT TO SIDE CHORD AT WL 195 ON AFT RIGHT SIDE OF BS 178 BULKHEAD HAS (1) MISSING/LOOSE FASTENER. REMOVED DAMAGED INTERCOSTAL; FORMED, LOCATED, DRILLED INTERCOSTAL IAW B737-300 SRM 51-40-02 PG 1; TREATED AND PRIMED IAW SRM 51-20-01 PG 1.SDR AWXA0001516Floorbeam · crackedFLOORBEAM LOWER ANGLE HAS ELONGATED/CRACKED FASTENER HOLES BS 178 RBL 24 WL 195. REMOVED FASTENERS; CUT OUT DAMAGE ON FLOORBEAM LOWER ANGLES; FORMED, CUT DRILLED AND INSTALLED REPAIR ANGLES AND FILLERS IAW B737-300 SRM 51-70-12 PG 1SDR AWXA0001515Doubler · crackedR1 DOOR JAMB, FWD UPPER CORNER BEAR STRAP INTERIOR SKIN HAS CRACK EMANATING FROM FIFTH FASTENER FROM TOP IN RADIUS. REMOVED FASTENERS, STOP DRILLED CRACK; FABBED AND INSTALLED REPAIR DUOBLERS IAW B737-300 SRM 51-40-02 PG 1 AND DWG 65C33800.SDR AWXA0001514Angle · elongatedFS 178 BULKHEAD AFT FACE FLOORBEAM LOWER ANGLE HAS ELONGATED HOLES WL 195 LBL 24. REMOVED FASTENERS, CUT OUT DAMAGE, FORMED, DRILLED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW B737-300 SRM 51-70-12 PG 1; HEAT TREATED ANGLES IAW TIMCO TPS-1003 REV A; TREATEDSDR AWXA0001513Floorbeam · corrodedCABIN FLOORBEAM UPPER CHORD UPPER SURFACE CORRODED AT BS 312 RBL 13 WL 208. REMOVED UPPER CHORD SECTION OF FLOORBEAM AT BS 312 BL 18L - 24R WL 208; LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION IAW B737-300 SRM 53-10-51 FIG 205.SDR AWXA0001512Frame · crackedLEFT SIDE CHORD AT WL 207 ON AFT SIDE OF BS 178 BULKHEAD CRACKED IN RADIUS. REMOVED LEFT SIDE WEB, REMOVED LEFT SIDE CHORD; LOCATED, DRILLED AND INSTALLED NEW SIDE CHORD IAW B737-300 SRM 51-40-02 PG 1 AND 10; REINSTALLED WEB IAW B737-300 SRM 51-40-02 PG 1 ANDSDR AWXA0001511Bulkhead · crackedFS 178 BULKHEAD WEB FROM FWD SIDE WL 234.1 CRACKED AT 4 FASTENERS RBL 9, 10.2, 11 AND 12. REMOVED FASTENERS; CUTOUT DAMAGED AREA; LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08 PG 265-269, FIG 209.SDR AWXA0001476Skin · gougedFUSELAGE SKIN AT L1 DOOR CUTOUT HAS NUMEROUS GOUGES AT FWD LWR CORNER. REPAIRED AREA IAW AWA ER 03-5310-01059-JS1 AND DWG 65C27257-5.SDR AWXA0001475Skin · crackedFUSELAGE SKIN AT L1 DOOR CUTOUT HAS CRACK EMANATING FROM FASTENER HOLE INTO RADIUS OF JAMB. REPAIRED CRACK IAW AWA ER 03-5310-01059-JS1 AND DWG 65C27257-5.SDR AWXA0001474Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 202 LBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTM PT 6 51-00-00. STOP DRILL TERMINATED CRACK; REPAIR PARTS FABBED AND INSTALLED IAW SRM 53-10-08.SDR AWXA0001473Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 202 RBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTM PT 6 51-00-00. CRACK TERMINATED; REPAIR PARTS FABBED AND INSTALLED IAW SRM 53-10-08.SDR AWXA0001472Web · crackedFLOOR WEB CRACKED FS 180 LBL 26 WL 207. REMOVED DAMAGED WEB IAW SRM 51-40-02; FABBED NEW WEB IAW DWG 65-45833; INSTALLED NEW WEB IAW SRM 51-40-02.SDR AWXA0001471Web · crackedFLOOR WEB CRACKED AT FS 180 RBL 26 WL 207. REMOVED DAMAGED WEB IAW SRM 51-40-02; FABBED NEW WEB IAW DWG 65-45833; INSTALLED NEW WEB IAW SRM 51-40-02.SDR AWXA0001470Web · crackedAFT CARGO DOOR WEB CUTOUT FOR THE ROD END IS CRACKED. STOP DRILLED CRACK IAW SRM 51-40-13; HFEC INSP IAW NTM PT.6 51-00-00 FIG 23. CRACK TERMINATED AT STOP DRILL; FABBED AND INSTALLED REPAIR DOUBLER ON AFT CARGO DOOR INNER WEB CUTOUT FOR LATCH ROD END IAW SR
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