N682CA, cancelled Sep 11, 2008
Service difficulty reports · 66
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 = 'N682CA' AND deregistration_id = 'N682CA-2008-09-11' 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 = 'N682CA' AND deregistration_id = 'N682CA-2008-09-11' 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 C1HA200682019Wire · broken"UPON RETRACTION OF FLAPS AFTER TAKEOFF, AMBER NR 7 LEADING EDGE LIGHT REMAINED ILLUMINATED, RUN COM PROCEDURE 2.27.12, DUMPED FUEL RETURN TO DEW. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER MM 27-81-32, OPS CHECK LEAK CHECK OK WHILE RARE ACTUATOR MX FOUND FOSDR C1HA200682018Shutoff Valve · failedAT FL350 THE NR 3 BLEED AIR TRIP OFF LT ILLUMINATED.THE RT DUCT PRESSURE NEEDLE DROPPED FROM APPROX 24 PSI TO 10 PSI AND THE CABIN STARTED TO CLIMB. COM 2.36.2 WAS PERFORMED,THE 33 BLEED AIR VALVE WAS CLOSED, AND THE RT DUCT PRESSURE REMAINED AT 10 PSI. THE NRSDR C1HA200682017Bleed Valve · failedAT FL350 THE NR 3 BLEED AIR TRIP OFF LT ILLUMINATED.THE RT DUCT PRESSURE NEEDLE DROPPED FROM APPROX 24 PSI TO 10 PSI AND THE CABIN STARTED TO CLIMB. COM 2.36.2 WAS PERFORMED,THE 33 BLEED AIR VALVE WAS CLOSED, AND THE RT DUCT PRESSURE REMAINED AT 10 PSI.THE NSDR C1HA200682006Seat Track · corrodedBS 1010-1070 LBL 45 CABIN SEAT TRACK CHANNEL HAS CORROSION & IS CRACKED ON O/B FLANGE BS 1070. REMOVED SEAT TRACK LBL 45 BS 1010-1070 IAW B727 SRM 51-30-2, FABRICATED SEAT TRACK USING BAC1520-792 7178-T6, DIM 79 INCHES IAW B727 SRM 53-10-1 FIG 7. ALODINE ANDSDR C1HA200682001Seat Track · corrodedBS 1010-1030 RBL 45 CABIN SEAT TRACK TOP & O/B FLANGE HAVE CORROSION. FOUND CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED DAMAGED TRACK FROM STA 950F TO 1030 RBL 45 IAW 727 SRM 51-30-7, FABRICATED NEW TRACK FROM BAC1570-792 7178 T6, DIM 80 INCHSDR C1HA200682002Beam · crackedSTA 1183 BULKHEAD, VERTICAL BEAM AT RBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-15, PER S/B 727-53-0192 FIG 2 REV 1 DATED MAY 30/91.SDR C1HA200682009Floorbeam · corrodedFLOORBEAM BS 344 HAS CORROSION. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA, FABBED FILLER, 7075-T6, .080, 1 X .1875 INCH (2EA) REPAIR ANGLES 7075-T6, .071, 16.5 X 1.875 INCH, & 2 EA SAME MAT 14.5 X 1.875 INCH IAW B727 SRM 53-10-2 FIG 7SDR C1HA200682007Floorbeam · corrodedBS 1030 RBL 4 - 10 LBL CABIN FLOOR SUPPORT UPPER FLANGE HAS CORROSION. CUT OUT DAMAGE AREA AT BS 1030 RBL 20 TO LBL 10 IAW B727 SRM 51-10-1, FABRICATED T-SUPPORT USING BAC1505-100617, DIM 43.125 X 2.25 INCH, 2 EA SUPPORT ANGLE AND TWO STRAP IAW B727 SRM 53-10SDR C1HA200682010Skin · bulgedFUSELAGE EXTERIOR BS 1075 STRINGER 29 RT AT FWD END OF REPAIR DOUBLER HAS SKIN BULGED WITH POPPED RIVET. CUT OUT DAMAGED SKIN, FABBED AND INSTALLED FILLER (2024-T3 .063, DIM 1.5 X 1 INCH) AND DOUBLER (2024-T3 .080, DIM 43.25 X 14.625 X .625 INCH) IAW 727 SRM SDR C1HA200682013Stringer · corrodedAFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1030 THRU BS 1050 CORROSION SPOTS BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED STRINGER, MATERIAL USED BAC1498-145, DIM 17 INCHES IN LENGTH IAW 727 SRM 53-10-3 FIG 1. NO CORROSION NOTEDSDR C1HA200682014Web · crackedRIGHT WHEEL WELL BS 870, WEB IS CRACKED FROM APU LOAD CONTROL VALVE ACCESS CUTOUT. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS, FABBED FROM 15-5 PH STEEL, DIM 21 X 18.5 INCHES AND 10.75 X 11.25 INCHES IAW 727 SRM 53-10-9 FIG 5.SDR C1HA200682016Floor Support · bulgedCOCKPIT FLOOR SUPPORT AT FS 303 & LBL 12 IS BULGED. REMOVED, FABBED NEW & INSTALLED FLOOR SUPPORT IAW B727 SRM 53-10-2 FIG 7 & 51-30-2.SDR C1HA200682012Stringer · corrodedAFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1010 THRU BS 1030 SPOT OF CORROSION BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED DAMAGED STRINGER, MATERIAL USED BAC1498-145, DIM 18 INCHES IN LENGTH IAW 727 SRM 53-10-3 FIG 1. NO CORROSDR C1HA200682005Seat Track · corrodedBS 1030-1090 LBL 24 CABIN SEAT TRACK O/B UPPER FLANGE IS CORRODED. REMOVED AND REPLACED SEAT TRACK LBL 24 BS 950-1090 WITH BAC 1520-792, DIM 129.5 INCH IAW 727 SRM 53-10-5 FIG 1.SDR C1HA200682004Vertical Beam · crackedSTA 1183 BULKHEAD, VERTICAL BEAM AT LBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-14, PER S/B 727-53-0192 FIG 2 REV 1 DATED MAY 30/91.SDR C1HA200682003Seat Track · corrodedBS 1030-1120 RBL 24 CABIN SEAT TRACK HAS SMALL AREAS OF CORROSION. REMOVED DAMAGE TRACK BS 1010 - 1130 RBL 24 IAW B727 SRM 51-30-2. FABRICATED NEW TRACK P/N BAC1520-7927178-T6, DIM 126 INCH FROM STA 1010 TO 1130 IAW B727 SRM 53-10-1 FIG 7. ALODINED AND PRIMSDR C1HA200682015Stiffener · crackedRIGHT WHEEL WELL BS 870 & KEEL BEAM VERTICAL STIFFENER CRACKED (NDT CONFIRMED). REMOVED AND REPLACED DAMAGED STIFFENER P/N 65-18636-378, IAW 727 SRM 51-30-2.SDR C1HA200682008Floorbeam · corrodedBS 1110 LBL 24 - RBL 24 TRANSVERSE FLOOR SUPPORT UPPER FLANGE HAS CORROSION (BOTH SIDES). REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. REMOVED LBL 24 TRACK IAW B727 SRM 51-30-2, FABRICATED T-ANGLE 60 INCH DIM 4 ES STRAP DIM 15", 11", 14" AND 10.5". FOUR EASDR C1HA200682011Stringer · corrodedAFT PIT STRINGER 29R CORRODED AT BS 1075. REMOVED AND REPLACED DAMAGED STRINGER SECTION MATERIAL USED BAC1498-147, DIM 18.375 INCH LENGTH IAW 727 SRM 53-10-2 FIG 9 & 53-10-3 FIG 1.SDR C1HA200582001Window · crackedENROUTE WINDOW CRACKED, REPLACED R2 WINDOW REF 56-12-11 AND AJUSTED AND OPS CK GOOD.SDR C1HA200482002Skin · delaminatedLEFT IB FORE FLAP DELAMINATED AT IB AFT EDGE. PIN 65-21630-249A REQ NR 125615 REMOVED AND REPLACED. LT IB FORE FLAP, OPS CHECKED OK IAW MM 27-51-01 RII ACCOMPLISHED FOR INSTALLATION AND OPS CHECKS.SDR C1HA200482001Switch · out of adjustAFTER TAKEOFF ON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT STAYED ILLUMINATED. RAN COM PROCEDURE 2.32.29. ADJUSTED RIGHT MLG DOOR SWITCH PER CHAMPION AIR MM 32-62-11, OPS CHECK NORMAL.SDR C1HA200382011Skin · crackedLOWER RUDDER TAB UPPER LEFT AND RIGHT SIDE IS DEBONDED AND CRACKED.SDR C1HA200382010Battery · inoperativeAFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES (2EA) FOR EMERGENCY EXIT IAW MM 33-50-71, OPS CHECKS GOOD.SDR C1HA200382009Engine · malfunctionedNR 2 ENG WAS FLUC EPR+- 4 N1, N2 EGT AND FUEL FLOW ALL WERE FLUCT. PRIOR TO SHUTDOWN NR 2 ENG FUEL HEAT ICING LIGHT STROBING EVEN WITH FUEL HEAT ON. ENG SHUT DOWN DURING FINAL CLIMB TO 37000 WHEN ENG SHUT DOWN ENG OIL CLIMBED TO 140 C ENG WINDMILLED FOR 37 MINSDR C1HA200382007Smoke Detector · malfunctionedSMOKE DETECTOR FWD LAV ACTIVATES OCCASIONALLY WHEN DOOR IS SHUT.SDR C1HA200382006Smoke Detector · will not testSMOKE DETECTOR IN FWD LAV WILL NOT TEST EVERY TIME.SDR CH1A200382005Compressor · stalledON APPROACH TO LAS AT 500FT, NR 2 ENGINE COMPRESSOR STALLED. DID NOT USE NR 2 REVERSER. FLT ATTND REPORTED COMP STALL ON ROLL OUTSDR C1HA200382004Fire Loop · out of positionNR 1 GROUND FAULT FIRE DETECTION SYSTEM LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 1 ENGINE FIRE LOOP IAW M/M 26-11-01 GRND OPS. CHECKS GOOD.SDR C1HA200382003Fire Loop · shortedNR 1 ENGINE FIRE WARNING GROUND FAULT DECTOR LIGHT ILLUMINATED DURING FLIGHT. PERFORMED FIRE WARNING TEST PROCEDURES COM 2.26.3 TESTED NORMAL REPOSITIONED FIRE LOOP GROUND TESTS NORMAL. PER MM 26-11-01SDR C1HA200382002Connector · disconnectedFIRE WARNING TEST FAILED NR 2 ENGINE "B" LOOP. INSPECTED FOUND CONNECTOR PLUG AT ENGINE LOOP DISCONNECTED. RE-CONNECTED OPS CHECK GOOD IN REF TO MM 26-11.SDR C1HA200382001Slide · dislodgedL2 DOOR SLIDE OUT OF CONTAINER. REINSTALLED L2 SLIDE IN CONTAINER IAW MM 26-60, OK FOR SERVICE.SDR C1HA200282018Battery PackLH FWD OVERWING EMERGENCY EXIT LIGHT INOPR&R L/H FWD EMERG EXIT LIGHT BATTERY PACK IAW MM 33-50-21, OPS CHECKS GOOD.SDR C1HA200282017BulbL-2 & R-2 EMERGENCY EXIT SIGNS INOPRELAMPED L-2 & R-2 EMERG EXIT LWR DOOR SIGNS IAW MM 33-50-11. OPS CHKS GOOD.SDR C1HA200282016BatteryAft Ceiling emergency exit sign INOPReplaced battery cartridge ASSY.SDR C1HA200282015O-Ring · leakingENGINE NR 3 OIL QUANTITY DROPPED TO 1.5 GALLONS. ENGINE OIL TEMPERATURE WAS 90 DEGREES, OIL PRESSURE WAS 44 AND OIL QUANTITY CONTINUED TO DROP TO .5 GALLONS. TEMPERATURE BEGAN TO RISE AND PRESSURE BEGAN TO DROP, EXECUTED A PRECAUTIONARY SHUTDOWN. FOUND O-RISDR C1HA200282014Cover · brokenLT MAIN GEAR LIGHT COVER BROKEN. RESECURED LIGHT COVER AS REQUIRED.SDR C1HA200282013Light · inoperativeEMERGENCY PORT LIGHT IN COCKPIT INOP. R&R LIGHT ASSY PER MM 33-50-101. OPS CK GOOD.SDR C1HA200282012Power Supply · dischargedLEFT WING CENTER EMERGENCY LIGHT COVERWING INOP. R&R BATTERY POWER SUPPLY IAW MM 33-50-22. ALL OPS CKS NORMAL.SDR C1HA200282011Warning System · activatedAMBER AIRSTAIR ANNUNCIATOR ILLUMINATED INFLIGHT. VISUAL INSPECTION FROM AFT ENTRY REVEALED DAYLIGHT FROM RIGHT AFT STAIR. DIVERTED TO ORD AND DUMPED FUEL. UPON ARRIVAL FOUND AIRSTAIR IN UP AND LOCKED POSITION. CHECKED OPERATIONS OF AIRSTAIRS PER MM. INSPESDR C1HA200282010Power Supply · dischargedFIXED INTERIOR EMERGENCY AREA LIGHTS AT AFT ENTRY INOP, 2 ROUND LIGHTS POINTING DOWN. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR AFT ENTRY IAW MM 33-50-71. EMERGENCY LIGHTS OPS CHECK GOOD.SDR C1HA200282009Access Door · corrodedCONDITIONED AIR GROUND CONNECT ACCESS DOOR HAS A BULGE IN SKIN AT HINGE POINT. (CORROSION RELATED C CHECK FINDING). DOOR REPLACED PER SRM.SDR C1HA200282008Panel · chafedRT WING UPPER I/B PANEL FOR APU EXHAUST LOUVER IS CHAFING INTO AFT I/B CORNER OF RECESSED PAN. (CORROSION RELATED C CHECK FINDING) PANEL REPLACED PER AMM.SDR C1HA200282007Seat Track · corrodedSEAT TRACK CHANNEL AT RBL 54 STA. 344 CORRODED (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM.SDR C1HA200282006Seat Track · corrodedSEAT TRACK AT RBL 44 STA 344 TO STA 460 HAS CORROSION. (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM.SDR C1HA200282005Tab · delaminatedLOWER RUDDER TAB HAS DELAMINATED ON LT UPPER FWD CORNER. (C CHECK FINDING) REPAIR APPROVED BY 8110.SDR C1HA200282004Splice · corrodedSTA 480 SPLICE PLATE HAS CORROSION AT FWD END OF INTERCOSTAL BETWEEN STR 28 LT & RT. (C CHECK FINDING) REPAIR APPROVED BY 8110SDR C1HA200282003Stringer · corrodedAFT PIT STR 29 LT CORRODED AT STA. 950 A. (C CHECK FINDING) REPAIR APPROVED BY 8110.SDR C1HA200282002Floor Support · corrodedFLOOR SUPPORT CORRODED STA. 1070 LBL 22-44. (C CHECK FINDING) REPAIRED PER SRMSDR C1HA200282001Stringer · corrodedSTA. 560 FWD SIDE OF TOP ANGLE IS EXFOLIATED ON O/B SIDE OF STR 26 RT, ALSO HAS ONE CORRODED FASTENER THRU WEB. (C CHECK FINDING) REPAIR APPROVED BY 8110.
Back to N682CA, cancelled Sep 11, 2008