N69348, cancelled Oct 8, 2009
Service difficulty reports · 47
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N69348' AND deregistration_id = 'N69348-2009-10-08' 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 n_number = 'N69348' AND deregistration_id = 'N69348-2009-10-08' 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 CALA2009070100342Charger · intermittentAFT EXIT DOOR EMERGENCY LIGHTS RIGHT AND LEFT SIDE ILUMINATED. REMOVED AND REPLACED BATTERY CHARGER, AND BATTERY PACK. OPS CHECKS GOOD.SDR CALA2008122301163Skin · crackedSTRINGER 24L, STATION 727E - 718 OUTER SKIN HAS 1 INCH CRACK. REPAIRED CRACK IN OUTER SKIN STRINGER 24L STATION 727 - 718 PER B737 SRM 53-00-01 FIG 201. TOTAL WEIGHT OF REPAIR, 9.84LBS FOR WEIGHT AND BALANCE CALCULATION.SDR CALA2008122201162Intercostal · corrodedFUSELAGE FRAME, SKIN AND SURROUNDING STRUCTURE CORRODED STATION 227.8 FROM LBL-12 TO RBL-12 (BILGE). REMOVED CORROSION FROM HORIZONTAL CHORD, FOUND TO BE WITHIN LIMITS, AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. CLEANED AREA AND INSTALLED NEW INTERCOSTAL PERSDR CALA2008122201159Skin · delaminatedRIGHT WING NR 5 SLAT TRAILING EDGE WEDGE INBOARD AND OUTBOARD PROTECTIVE FINISH FOUND DELAMINATION ON OUTBOARD TRAILING EDGE. FABRICATED REPAIR DOUBLER AND REPLACED DAMAGED HONEYCOMB. BONDED REPAIR DOUBLER AND CORE, SEALED INBOARD AND OUTBOARD TRAILING EDGE SDR CALA2008121901153Skin · delaminatedLEFT WING NR 3 SLAT INBOARD END SKIN IS DELAMINATED. REPAIRED LEFT WING NR 3 SLAT TRAILING EDGE WEDGE PER SRM 51-70-10.SDR CALA2008121901152Floorbeam · crackedFLOORBEAM BS 328 LBL 12 UPPER TEE CAP CRACKED SL-7 69. REPAIRED CRACKED FLOORBEAM AT BS 328 LBL 12 UPPER TEE CAP PER SRM 53-10-51 FIG 201.SDR CALA2008121101138Door Frame · crackedFORWARD CARGO DOOR CUTOUT FORWARD FRAME CRACKED AT LOWER DOOR STOP FITTING AT STR 24R. REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT FORWARD FRAME PER SRM 51-10-2, PAGE 8, MAT ID 65-20722U70, PAC 59980.SDR CALA0800700Skin · corrodedGENERATED DIP DUE TO HEAVY CORROSION AT STATION 967, STR 27LT TO STR 27RT, PERFORM A PERMANET REPAIR PER EC/RA 5331-01244 WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS, WHICHEVER OCCURS FIRST. DURING OPEN-UP FOUND MORE CORROSION, REMOVED EXISTING REPAIRS AND REPAIRSDR CALA0700525Actuator · inoperativeTHE LEFT MLG DID NOT INDICATE DOWN & LOCKED WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. MANUAL EXTENSION WAS PERFORMED AND YAW WAS FELT WHEN LEFT MAIN EXTENDED. THE GEAR INDICATED 3 GREEN AND LANDING WAS NORMAL. THE GEAR WAS SWUNG SEVERAL TIMES WITH NO FAULSDR CALA0700490Controller · inoperativeTHE CREW RECEIVED A CABIN ALTITUDE WARNING CLIMBING THROUGH FL 270. THE QRH WAS FOLLOWED AND A RAPID DESCENT TO 13,000 FEET WAS ACCOMPLISHED. CABIN PRESSURE WAS RECOVERED VIA MANUAL DC. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLESDR CALA0600239Brace · corrodedINSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE RT LOWER I/B CHORD CORRODED BETWEEN STA 1104 AND 1112. THE AREA WAS REPAIRED IAW ECRA 5510-01840.SDR CALA0600238Frame · corrodedINSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE LT LOWER I/B CHORD CORRODED BETWEEN STA 1121 AND 1129. THE AREA WAS REPAIRED IAW ECRA 5510-01841.SDR CALA0600237Skin · corrodedINSPECTION FOUND CORROSION ON AFT INTERIOR SURFACE OF THE LT WING AFT FUEL BOOST PUMP SKIN CUTOUT AT WS 70.85-140. A REPAIR WAS INSTALLED IAW ECRA 5720-01990.SDR CALA0600236Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 967, S27R. A SKIN REPAIR WAS INSTALLED IAW ECRA 5331-01244.SDR CALA0600228Floorbeam · crackedINSPECTION FOUND A 1.25 INCH CRACK ON THE TOP EDGE OF FLOORBEAM WEB AT STA 328, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01373.SDR CALA0600227Stringer · crackedINSPECTION FOUND A 1 INCH CRACK AT FORWARD PASSENGER DOOR CUTOUT ON STRINGER 15L SPLICE CHANNEL, STA 360, LBL 50. THE STRINGER WAS REPAIRED IAW ECRA 5311-01259 AND A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 6,000 FLIGHT CYCLES.SDR CALA0600297Skin · crackedINSPECTION FOUND A CRACK AT THREE EACH LIGHTENING HOLES ON THE INNER SKIN OF THE FORWARD CARGO DOOR. THE SKIN WAS REPAIRED IAW ECRA 5232-01076.SDR CALA0600223Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 765 JUST ABOVE STRINGER 21R ON BONDED DOUBLER LINE. THE CRACKED SECTION OF SKIN WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-0, REPAIR 31, PROCEDURE V, DETAIL VII, FIGURE 201, PAGE 228.SDR CALA0600221Floorbeam · corrodedINSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11-36. REPLACED T-CAP ON FLOORBEAM IAW SRM 53-10-5, REPAIR 5.SDR CALA0600218Beltframe · corrodedINSPECTION FOUND FORWARD BAGGAGE BIN BELT FRAME CORRODED AT STA 500D, S27L, LBL11-13. A DOUBLER WAS INSTALLED IAW SRM 53-00-07 FIGURE 201 REPAIR 7.SDR CALA0600217Beltframe · corrodedINSPECTION FOUND FORWARD BAGGAGE BIN BELT FRAME CORRODED AT STA 480, S27L, LBL 13-17. REPAIRED IAW SRM 53-00-07.SDR CALA0600214Angle · corrodedINSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 947-999, LBL 40. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0600224Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN THE FORWARD CARGO DOOR LOWER CORNER FRAME JUST BELOW DOOR HOLD OPEN HOOK. THE DOOR FRAME WAS REPAIRED IAW SRM 51-40-02 AND EA 5230-01030.SDR CALA0500324Wire · shortedTHE FIRST CLASS EMERGENCY ESCAPE AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE FOUND SHORTED WIRING TO TRANSFORMER. THE WIRING WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD.SDR CALA0400713Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BELOW FASTENER ROW BETWEEN STA 727E AND 747, S24R. A REPAIR DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 229.SDR CALA0400584Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AND CRACKED AT STA 259.5-360, S24L TO S29L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5310-04421.SDR CALA0400535Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 747, STRINGER 23L. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 229.SDR CALA0300044Skin · crackedINSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN AT STA 727A, S23L. REPAIRED IAW ECRA 5330-03090.SDR CALA0200352Keelbeam · corrodedINSPECTION FOUND KEEL BEAM LT LOWER O/B CHORD CORRODED AT STA 727. REPAIRED IAW ECRA 5311-01127.SDR CALA0200351Skin · crackedINSPECTION FOUND #6 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01.SDR CALA0200339Seat Track · corrodedINSPECTION FOUND MAIN CABIN FLOOR R/H I/B SEAT TRACK HAD CORROSION AND WORN LOBES AT BS 787 AND 797, THE CORRODED AND WORN SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK SECTION WAS SPLICED IN IAW SRM 53-00-52, FIGURE 204.SDR CALA0200337Seat Track · corrodedINSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-940. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.SDR CALA0200335Seat Track · corrodedINSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 907-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52.SDR CALA0200332Strap · corrodedINSPECTION FOUND R/H SIDE Y STRAP CORRODED FROM STA 1006 TO AFT PRESSURE BULKHEAD, RBL 6. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0200331Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT UNDER R2 DOOR Z-ANGLE AT STA 969 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND 51-30-01.SDR CALA0200330Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0000552Harness · brokenEMERGENCY AISLE PATH LIGHTING INOP AT ROW 6 AND 22. REPLACED WIRE HARNESS AT BOTH ROWS PER MAINTENANCE MANUAL 33-51-02 PG 501.SDR CALA9900540Trigger · out of positionFORWARD ENTRY DOOR WILL NOT OPEN. FOUND RELEASE LATCH MECHANISM DISSASSEMBLED AND TRIGGER OUT OF POSITION. REASSEMBLED AND TESTED PER MM 52-11-00 PAGE 501.SDR CALA9801501Stringer · corrodedINSPECTION FOUND STRINGER CORRODED JUST BELOW RT AFT LAV DUMP CHUTE FROM STA 1006 TO 1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER AND SHIM WERE FABRICATED AND INSTALLED IAW ECRA 5360-01018.SDR CALA9801487Floorbeam · corrodedINSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344, LBL 30 TO 20. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.SDR CALA9801486Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 15 AND LBL 20. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-10-51.SDR CALA9800721Oven · dirtyTHE CREW REPORTED SMOKE COMING FROM NR 1 AND NR 2 AFT GALLEY OVENS IN FLIGHT. THE SMOKE WAS MOMENTARY. THE FLIGHT WAS CONTINUED TO DEN WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. FOOD RESIDUE WAS FOUND ON THE HEATING ELEMENTS OF BOTH OVSDR CALA9800016Logic Card · inoperativeTHE RT MLG INDICATION WAS SHOWING RED AND GREEN AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. MAINTENANCE FOUND THE M986 LOGIC CARD AT FAULT. THE M986 LOGIC CARD WAS REMOVSDR CALA9701711Tire · failedA LT MLG TIRE BLEW ON TAKEOFF, THE A-HYD SYSTEM PRESSURE AND QUANTITY WAS LOST. THE AIRCRAFT WAS RETURNED. UPON LANDING THE OTHER LT MLG TIRE BLEW. THE BLOWN TIRES HAD DAMAGED THE LEFT INBOARD AFT FLAP, THE LT INBOARD MLG DOOR, THE LEFT GEAR DOWNLOCK AFT SPSDR CALA9700971Windshield · failedA STRONG ODOR ACCOMPANIED BY SMOKE WAS OBSERVED IN THE COCKPIT DURING CLIMB-OUT OF DTW ENROUTE TO EWR. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FIRST OFFICER'S NR 5 WINDOW OVERHEATING AND CAUSING THE ODOR AND SMOSDR CALA9601302Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 540, STRINGER 22R. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-11.SDR CAL960191Rollers/Tracks · lack of lubeFLT NR 1708 - EWR - WHEN FLAPS WERE SELECTED BEYOND 5 DEGREES CREW RECEIVED T/E FLAP ASYMMETRY. THE SAFETY WIRES WERE BROKEN ON GPWS AND ALTERNATE FLAP MASTER SWITCH. THE LEFT INDICATOR WENT TO 10 DEGREES AND THE RIGHT STAYED AT 5 DEGREES. THE AIRCRAFT WAS
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