N73751, cancelled Aug 9, 2006
Service difficulty reports · 122
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 = 'N73751' AND deregistration_id = 'N73751-2006-08-09' 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 = 'N73751' AND deregistration_id = 'N73751-2006-08-09' 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 XN0A1311Strut · lowON TAXI OUT, KNOCKING SOUND FROM NOSE GEAR. SERVICED NOSE STRUT WITH NITROGEN IAW B727 MM CHAPTER 12-20-00.SDR XN0A1286Relief Valve · out of adjustNR 1 ENGINE OIL PRESSURE WENT TO REDLINE ON THROTTLE. TO TAKEOFF POWER. ADJUSTED OIL PRESSURE RELIEF VALVE TO 43 PSI AT IDLE IAW MM 72-00. OPS AND LEAK CHECKS GOOD AT IDLE. (ORIG/CLOSED)SDR XN0A1283Strut · lowON TAXI OUT THE NOSE GEAR SEEMED TO BOTTOM OUT. INSPECTED NOSE STRUT ASSY AND FOUND STRUT LOW ON NITROGEN, SERVICED NLG STRUT WITH NITROGEN IAW B727 MM CHAPTER 32-10-00.SDR XN0A1278Wire · looseSPEED BRAKE/ FLAP WARNING WILL NOT TEST IN TAXI OUT AND T/O WARNING HORN. SECURED LOOSE WIRE ON AURAL WARN CB. CHECKS GOOD ON GROUND.SDR XN0A1270Transmitter · malfunctionedCREW O2 TO 0 PSI IN TAXI OUT SWF, BACK TO THE RAMP. RESET PRESS TRANSMITTER ON CREW BOTTLE, CHECK GOOD IAW 35-11-00.SDR XNOA1187Warning System · activatedMAIN CARGO AND LOWER CARGO WARNING IN FLIGHT WITH LIGHT AND BELL.SDR CALA9801959Wire · brokenEMERGENCY AISLE PATH LIGHTING INOP AT ROW 10 ABC. FOUND BROKEN WIRE AT LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01.SDR CALA9800576Skin · debondingINSPECTION FOUND RT WING NR 6 KRUEGER FLAP DEBONDING. A REPAIR WAS ACCOMPLISHED IAW ECRA 5720-01064.SDR CALA9800575Floorbeam · corrodedINSPECTION FOUND TOP FLANGE OF FLOORBEAM CORRODED AT FS 1110, RBL 10 TO RBL 63. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9800574Seat Track · corrodedINSPECTION FOUND TOP AND BOTTOM OF RT OUTBOARD SEAT TRACK CORRODED AT FS 400 TO 440. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2, 53-10-5 AND 51-10-2.SDR CALA9800572Skin · gougedINSPECTION FOUND A 1 INCH GOUGE IN RT INBOARD FOREFLAP OUTBORD LEADING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED.SDR CALA9800570Flap Track · corrodedINSPECTION FOUND NR 7 FLAP TRACK AFT MOUNT CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0.SDR CALA9800569Floorbeam · corrodedINSPECTION FOUND TOP FLANGE UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED AT FS 360, RBL 10 TO LBL 18. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.SDR CALA9800568Chord · corrodedINSPECTION FOUND TOP AND BOTTOM OF CHORD CORRODED AT FS 310 TO 362, LBL 56. ALSO, DOUBLER AT FS 360 HAD A .5 INCH CRACK. THE CHORD WAS REMOVED, CORROSION WAS REMOVED FROM AREA IAW SRM 51-10-6. A NEW DOUBLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 5SDR CALA9800567Circumferential · crackedINSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT BS 804.5, S15R. THE CRACKED AREA WAS REMOVED, A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3.SDR CALA9800566Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING STA 656.50 STRINGER ON TOP OF CHORD RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW EA 5762-01050.SDR CALA9800565Skin · erodedINSPECTION FOUND RT SIDE OF LOWER RUDDER SKIN EDGE ERODED JUST ABOVE PANEL NR 9901. THE AREA WAS SANDED AND A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-40-8.SDR CALA9800564Skin · crackedINSPECTION FOUND A .1875 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075.SDR CALA9800563Skin · deterioratedINSPECTION FOUND LT LOWER SIDE OF UPPER RUDDER TAB FIBERGLASS REPAIR DETERIORATED. THE FIBERGLASS REPAIR WAS SANDED, REWORKED, AND PRIMED IAW SRM 51-40-9 AND 51-10-6.SDR CALA9800562Skin · crackedINSPECTION FOUND A .625 INCH CRACK THROUGH FASTENER AT R-1 DOOR OUTER SKIN LOWER FORWARD CORNER ABOVE GATE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-40-1.SDR CALA9800561Angle · crackedINSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.SDR CALA9800560Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN J-ANGLE SUPPORT ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. A REPAIR CHANNEL WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914.SDR CALA9800559Flap Track · corrodedINSPECTION FOUND UPPER MOUNT FLANGE OF NR 6 FLAP TRACK CORRODED AT FORWARD ATTACH CLEVIS. THE FLAP TRACK WAS REMOVED AND REPLACED.SDR CALA9800558Attach Fitting · corrodedINSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING AT BOTTOM OF WING CORRODED AT INBOARD FACE. THE FITTING WAS REMOVED AND REPLACED IAW OVERHAUL MANUAL 20-50-01.SDR CALA9800557Angle · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT BOLT HOLES OF LT WING LOWER LEADING EDGE SUPPORT ANGLE AT FS 120. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9800556Stiffener · crackedINSPECTION FOUND A .625 INCH CRACK IN STIFFENER AT BOTTOM OF LT WING LEADING EDGE RIB, WBL 92.0. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9800555Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0.SDR CALA9800554Skin · dentedINSPECTION FOUND RT OUTBOARD AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED.SDR CALA9800553Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL SUPPORT T-ANGLE. THE CRACK WAS LOCATED AT INBOARD AFT END, OUTBOARD OF NR 1 FLAP JACKSCREW. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-SDR CALA9800552Floorbeam · corrodedINSPECTION FOUND FLOORBEAM TOP FLANGE UPPER AND LOWER SURFACE CORRODED AT FS 360, RBL 10 TO LBL 10. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.SDR CALA9800551Skin · puncturedINSPECTION FOUND A HOLE IN RT OUTBOARD FOREFLAP UPPER INBOARD SURFACE. THE DAMAGED AREA WAS CUTOUT AND A HOT BONDED REPAIR WAS APPLIED IAW SRM 51-40-6 AND 51-10-6.SDR CALA9800550Flap Track · corrodedINSPECTION FOUND RT WING NR 7 FLAP TRACK FORWARD LUGS CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0.SDR CALA9800549Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.SDR CALA9800548Rib · wornINSPECTION FOUND VERTICAL STABILIZER NR 7 RIB WORN AT STRINGER 2R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.SDR CALA9800547Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN LT VERTICAL STABILIZER AT STA 1253, JUST ABOVE AND AFT OF PANEL NR 9523. THREE 1 INCH CRACKS WERE FOUND IN THE LT VERTICAL STABILIZER AT STA 1264. THE CRACKED AREAS WERE CUTOUT IAW SRM 54-10-1. FILLER AND DOUBLER REPAIRS WSDR CALA9800546Bulkhead Panel · crackedINSPECTION FOUND THE NLG WHEEL WELL FORWARD BULKHEAD TOP RIGHT PANEL, TOP LEFT PANEL, AND TOP CENTER PANELS CRACKED AT FASTENER HOLES. THE CRACKS WERE .5 TO 1 IN LENGTH. THE CRACKED AREAS WERE CUTOUT IAW SRM 51-40-2. REPAIR DOUBLERS AND FILLERS WERE FABRICASDR CALA9800545Skin · crackedINSPECTION FOUND A .5 INCH CRACK WITH DENT IN AFT BAGGAGE COMPARTMENT DOOR SKIN 23 DOWN FROM TOP AND 16 AFT. THE DENTED AND CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3.SDR CALA9800544Skin · dentedINSPECTION FOUND C-2 CARGO DOOR AFT LOWER EDGE BENT AND CORRODED. THE AFT LOWER FRAME SECTION WAS REMOVED IAW SRM 51-30-2 AND THE SKIN WAS STRAIGHTENED IAW SRM 51-40-1. THE NEW LOWER AFT FRAME SECTION WAS SEALED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9800543Frame · corrodedINSPECTION FOUND FLOOR MOUNT FRAME CORRODED AT AFT BIN STA 1148 TO 1166 BETWEEN STRINGER 26 TO 27R. A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-40-5 AND SRM 51-30-2.SDR CALA9800542Spar Web · crackedINSPECTION FOUND A 4 INCH CRACK IN CENTER WING SECTION AT REAR SPAR WEB UPPER RADIUS ABOVE PRODUCTION PANEL FROM RBL 0 TO RBL 4. THE AREA WAS REPAIRED IAW EA SA004-5710-01843, DRAWING 65C37620, AND SERVICE BULLETIN 727-57A0182.SDR CALA9800541Radome · erodedINSPECTION FOUND THE RADOME EXTERIOR SKIN HAD SOME SPOTS OF EROSION AND A SMALL HOLE. THE RADOME WAS REMOVED AND REPLACED IAW MM 53-15-0.SDR CALA9800540Rib · crackedINSPECTION FOUND A .25 INCH CRACK FROM END OF STRINGER ON TOP OF RIB, SECOND UPPER STRINGER FROM AFT SPAR, WS 656.50, ACCESS 7217. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-01050.SDR CALA9800539Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL SUPPORT RIB JUST INBOARD OF NR 3 SPOILER ACTUATOR IN FLAP COVE AREA. THE RIB SUPPORT WAS REMOVED, NEW PARTS WERE INSTALLED IAW SRM 51-10-6 AND 51-10-1.SDR CALA9800535Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL OUTBOARD SUPPORT RIB JUST INBOARD NR 4 SPOILER ACTUATOR IN FLAP COVE AREA. THE RIB AND ROD WERE REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9800534Skin · corrodedINSPECTION FOUND BOTTOM OF LT WING NR 7 SPOILER CORRODED. THE SPOILER WAS REPAIRED BY AVIATION COMPOSITES AND IAW WORK CARD 07-5750-1-2717..SDR CALA9800533Skin · separatedINSPECTION FOUND THE LT ELEVATOR CONTROL TAB INBOARD CORNER SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.SDR CALA9800532Skin · separatedINSPECTION FOUND THE RT ELEVATOR CONTROL TAB TRAILING EDGE SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.SDR CALA9800531Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 846, RBL 1. THE FLOOR SUPPORT WAS REMOVED. A DOUBLER AND FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-1.SDR CALA9800530Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, AND 53-10-3, PAGE 43, DETAIL 11.SDR CALA9800529Subfloor · corrodedINSPECTION FOUND FORWARD LAV OUTBOARD SUBFLOOR CORRODED AT FS 294-344, RBL 43-63. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED IAW SRM 51-10-1.
Back to N73751, cancelled Aug 9, 2006