N75851
Service difficulty reports · 119
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 = 'N75851' AND registry_match = 'registration' 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 = 'N75851' AND registry_match = 'registration' 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 CALA2019111601972Support Angle · cracked(B757-52-3-103) FWD CARGO DOOR UPPER AFT CORNER ANGLE SUPPORT IS CRACKED AS MARKED (114-02) REF ST-ENG N/R 0077385 REMOVED AND REPLACED FWD CARGO DOOR UPPER AFT CORNER ANGLE SUPPO RT; P/N: 6-53919U5, BATCH NO. 0003572579, P.O. NO. DAG1920450 IA W BOEING DRAWINSDR CALA2019111101961Gate · corrodedL2 DOOR LWR GATE HAS CORROSION ALONG OUTER EDGE. REF ST-SAA NR 0 077375. FOUND L2 DOOR LWR GATE OUT OF LIMITS IAW B757-3 SRM 52-10-02 L=4 .0 D=.150. REMOVED LOCATED AND INSTALLED NEW L2 DOOR LWR GATE PN 143N6106-45 IAW B757-3 SRM 51-40-02 AND DWG 143N6100. WORSDR CALA2019111101960Skin · dentedCUSTOMER SERVICE REPORTS DENT NEAR L2 DOOR. DENT IS BETWEEN STRINGER 15 AND 16 AT STATION 392.25. MEASURED DENT LOCATED BETWEEN STR 15 AND 16 L AND B.S.392 DENT MEASURES 4.625L X3.25 W WITH A DEPTH OF .140 A/Y= 3.25/.140=23.2, AND IS NOT WITH IN THE ALLOWABLE SDR CALA2019111601968Stringer · crackedSTRINGER 16L IN MAIN CABIN HAS A CRACK AT STA 780+24. REF ST-SAA NR 0077728. REMOVED, FABRICATED, AND INSTALLED STRINGER 16L FROM STA 780 TO 780+24, P/N: VTSAA143N3110-478 IAW BOEING DRAWING 143N3500 REV 3 ACCOMPLISHED COMPLETED AND ACCEPTED.SDR CALA2019111101953Stringer · crackedB757-53-3-0559 STRINGER 16R IN MAIN CABIN, HAS A CRACK AT STA 78 0+24. (96-23) REF ST-ENG N/R 0077730 REMOVED, FABRICATED, AND INSTALLED STRINGER 16R IN MAIN CABIN FR OM STA 780 TO 780+24, P/N: VTSAA143N3110-478, IAW BOEING DRAWING 143N3500 REV F.SDR CALA2019110981928Crease Beam · corrodedB757-53-3-0563 CORROSION ON MAIN CABIN CREASE BEAM INNER CHORD U PPER SURFACE AT STA 733 RBL-63. RG1. REF ST-ENG N/R 0077772 REMOVED AND REPLACED CREASE BEAM INNER CHORD MAIN CABIN ST660 TH RU STA 760 RBL-63 IAW B757-3 SRM 51-40-02 AND BOEING DWG: PL143N 8322 SDR CALA2019110981927Skin · corrodedB757-49-3-8084 APU AIR INLET HOUSING TO FUSLAGE CUTOUT LANDING H AS AREAS OF CORROSION AS VIEWED THRU ACCESS 311AL RL076. REF ST- ENG N/R 0077683. BLENDED AND CHECKED LIMITS TO CORROSION ON APU INLET HOUSING TO FUSLAGE CUTOUT LANDING; L=20.5", W=1.25", D=.052"SDR CALA2019110981926Stringer · crackedB757-53-3-0556 STRINGER 16L IN MAIN CABIN HAS A CRACK AT STA 780 +36. (96-22) REF ST-ENG N/R 0077729 TRIMMED-OUT CRACK ON STRINGER 161 AT STA 780+36 (0.9"LONGX0.750" WIDEX0.25"R) AND ACCOMPLISHED A CATEGORY "A" PERMANENT REPAIR IA W B757-300 53-30-03 REPAIR 1 SDR CALA2019081601374Slide · unsecureDOOR-MOUNTED ESCAPE SYSTEM DOOR 2L - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS, D RING AT DOOR 2L DROPS BEHIND SLIDE PACK DUE TO DAMAGED TRIM. REINSTALLED TRIM AND INSTALLED NEW HOOK AND LOOP ON D RING.SDR CALA2019032500473Screw · missingMETAL STIFFNER RIGHT INBOARD CANOE OUTBOARD SIDE MISSING SCREW. ADDING THE PART DEPART ACFT NOTATION RESECURED WITH NEW SCREW. REF IPC 27-51-30-01.SDR CALA2018112302409Skin · corrodedCORROSION FOUND ON EXTERNAL SKIN AROUND AFT LAVATORY SERVICE DOOR FRAME. REF. AAR N/R:9725921 ACCOMPLISHED REAPAIR AT LAV SERVICE PANEL CUT OUT BEWEEN STA1540 & 1560 STRINGER 27R - ,29R AS PER U.A.L EC/RA#5331-02300 REV - ( FOR FURTHER DETAILS SEE PARTIAL WORSDR CALA2018011900236Battery · inoperativeEMERGENCY LIGHTS OUT AT SEAT 25, 26 & 27. ABC. R & R THE BATTERY CHARGER AND BATTERY M11082 AT BS 1334 ABOVE THE L3 DOOR IAW AMM 33-51-07. OPS CHECKED GOOD.SDR CALA2018011200156Power Supply · inoperativeROW 25, 26, & 27 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW WD 33-51-22.SDR CALA2018010500056Light · intermittentEMERGENCY LIGHTS INTERMITTENT AT VARIOUS LOCATIONS. RESET THE SYSTEM FIM 33-51. TEST OK IAW AMM 33-51-00-7150-044.SDR CALA2017122304574Duct · damagedLEFT ENGINE OVERHEAT ILLUMINATED, FOLLOWED QRH. NO ENGINE SHUTDOWN. EMERGENCY DECLARED. RIGHT ENGINE DUCT HAS A HOLE. REMOVED AND REPLACED RT ENGINE DUCT IAW 36-11-01 404-109-001. PERFORMED ENGINE RUNS, OPS CHECKED GOOD IAW 26-12-00-300-802C1.SDR CALA2017111704069Fitting · galledSTATUS MESSAGE FOR THE LT STRUT OVERHEAT DETECTOR 1. EMERGENCY DECLARED. REPLACED PRSOV IAW AMM 36-11-09. FOUND PNEU FITTING ON VALVE GALLED. NO LEAKS NOTED WITH DUCTS PRESSURIZED IAW AMM 36-11-09, ACCOMPLISHED ENGINE RUNS 80 PERCENT N1, 10 MINUTES, NO STSDR CALA2017111003968Duct · leakingSTATUS MESSAGE FOR THE LT STRUT OVERHEAT DETECTOR NR 1. EMERGENCY DECLARED. ACCOMPLISHED FIM 26-12-00-300-802C1. FOUND A LEAK IN THE Y DUCT IN THE LEADING EDGE ABOVE THE NR 1 PYLON. REMOVED AND REPLACED THE DUCT IAW AMM 36-11-01-004-083-001.SDR CALA2017110603945Engine · overtempEGT R ENG EEC EGT 984 15 SEC, REMOVED AND REPLACED NR 2 ENG DUE TO OVER TEMP. IAW AMM BOOTSTRAP METHOD REMOVAL AMM 71-00-020004-002-R00 INSTALLATION AMM 71-00-02-404-003-R00. OPS CHECK GOOD A/C OK FOR SERVICE.SDR CALA2017103003864Lens · missingOVERHEAD EMERGENCY LIGHT LENS AT SEAT 21ABC IS MISSING. INSTALLED NEW STOWBIN EMERGENCY LIGHT LENS LOCATED AT SEAT 21ABC.SDR CALA2017080802539Sensor · dirtyR1 DOOR SHOWS DISARMED BUT SLIDE LIGHT STILL ILLUMINATED. CLEANED THE SENSORS AND OPS CHECKED IAW AMM 52-11-00-206-021. SLIDE LIGHT CHECKED GOOD.SDR CALA2017080802532Sensor · contaminatedL1 DOOR SLIDE LIGHT INDICATOR FLICKERING INTERMITTENTLY ON AND OFF. CLEANED EXCESS GREASE FROM GIRT BAR SLIDE LOCKS. FOUND SLIDE LED INDICATOR CAP ONLY LIGHTING UP ON ONE SIDE. REPLACED LIGHT CAP. OPS CHECKED NORMAL.SDR CALA2017080802524Switch · malfunctionedR1 DOOR SLIDE LIGHT ON WITH DOOR DISARMED. CYCLE SLIDE ARM SWITCH, CLEARED FAULT. OPS TESTED GOOD...SDR CALA2017072402361Girt Bar · dirtyR1 DOOR SLIDE WILL NOT DISARM. CLEANED THE GIRT BAR RECEPTACLES.OPERATED DOOR AND ARMING MECHANISM IAW AMM 52-11-00-206-021.DOOR ARMING SYSTEM CHECKED GOOD.SDR CALA2017072402360Girt Bar · contaminatedSLIDE ARMED LIGHT AT 1L INTERMITTENT CLEANED GREASE FROM GIRT BAR RECEPTACLES.OPERATED DOOR & ARMING SYSTEM IAW AMM 52-11-00-206-021.ARM INDICATION LIGHT CKS GOOD.SDR CALA2017072102320Sensor · sticks1R SLIDE LIGHT REMAINS ILLUMINATED SLIDE WAS NOT ARMED WITH LIGHT ON. TAPPED SENSORS AT DOOR SILL AND LIGHT WENT OUT. OPS CHECKED SEVERAL TIMES WITH SUCCESS.SDR CALA2017071702268Battery Pack · dischargedWITH NO GND POWER DUE TO RAMP CLOSURE, THE EMER EXIT LIGHTS ON. SWITCH DID NOT WORK. REMOVED AND REPLACED BATTERY PACK AT M731 PER AMM 33-51-07, BATTERY PACK CAPACITY TEST GOOD.SDR CALA2017071402234Socket · dirty1R SLIDE LIGHT DID NOT COME OFF. CLEANED DOOR 1R SLIDE LIGHT SOCKET, OPS CK GOOD.SDR CALA2017061901908Light · not seatedDOOR 1R WILL NOT DISARM. SLIDE LT ILLUMINATED RESEATED LIGHT CAP.SDR CALA2017060901774Light · missingSLIDE LIGHT MISSING ABOVE DOOR 1R REPLACE SLIDE ARM LIGHT INDICATOR. TESTED PER TASK 25-66-01 PARAGRAPH I6.SDR CALA2017042101053Governor · faultyNR 2 ENGINE FAILED TO SPOOL TO TAKEOFF POWER. HUNG AT 1.43 EPR. REMOVED AND REPLACED THE NR 2 ENGINE FUEL FLOW GOVERNOR IAW AMM TASK 73-21-01-404-013. OPS AND LEAK CHECKED GOOD.SDR CALA2017012100147Fan · faultySMOKE IN BACK OF AIRPLANE. ODOR NOTED IN COCKPIT. SMOKE DISSIPATED AFTER RECIR FAN OFF. REPLACED LT RECIRC FAN. RAN PACKS, NO SMOKE OR ODOR NOTED IN CABIN OR COCKPIT.SDR CALA2016090600624Flap System · warning messageTE FLAPS DISAGREE EICAS DURING APPROACH, EXTENDED WITH ALTERNATE SYS LANDED WITH FLAPS AT 20. BITE TEST OF EFCU, NO EXISTING FAULTS. CYCLED FLAP HYDRAULICLY SEVERAL TIMES NO FAULTS NOTED. IAW AMM 27-51-00SDR CALA2015071700575Unknown · odorON CLIMB OUT, BELOW 1500 MSL, CABIN TEAM REPORTED STRONG ELEC BURNING SMELL AT DOOR 1 LT & RT WITH SIMILAR AT 2L & 2R. FLIGHT DECK CREW SMELLED IT AS WELL. CABIN REPORTED NO VENTS TURNED ON, LANDED ASAP. IAW AMM 05-51-58-910-801C, INSPECTED AS REQUIRED & STSDR CALA2015013000073Unknown · odorSTRONG ACRID ELEC SMOLDERING SMELL NEAR DOOR 4L. LANDED, FIRE CREW REPORTS THERMAL HOT SPOT IN WALL. AFTER VERIFICATION WITH FLIGHT CREW & FIRE DEPT AT AIRPORT NO HOT SPOTS DETECTED AT DOOR 4L, NOR ON FUSELAGE. PERFORMED ODOR & SMOKE INSPECTION IAW AMM 05-5SDR CALA2013111300842Angle · corrodedCORROSION AROUND FASTENERS IN AFT CARGO DOORWAY LOWER SILL LOWER ANGLE AT BS 1400 - 1420 RBL 23. REPAIRED IAW ECRA 5300-01791.SDR CALA2013111300844Skin · gougedB757-53-3-0527 FUSELAGE EXTERIOR BS 1340 TO BS 1360 AT STRINGER 25R SKIN GOUGED TWO PLACES. REPAIRED EXTERIOR FUSELAGE SKIN AT BS 1340 TO BS 1360 AT STRINGER 25 R IAW B757-300 SRM 53-00-01 FIG 201 REPAIR 2.SDR CALA2013111300841Frame · corrodedB757-53-3-0526 AFT CARGO FWD SIDE OF FRAME BS 1460 FROM BL 0 TO RBL 20 HAS CORROSION. REMOVED CORROSION FROM FWD SIDE OF FRAME AT BS 1460 FROM BL 0 TO RBL 20. ORIGINAL MATERIAL .063, DEEPEST AREA OF CORROSION REMOVED WAS .025 W.038, MATERIAL REMAINING FRAMESDR CALA2013111300835Gate · corrodedCORROSION ON L2 DOOR LOWER GATE EDGE. REMOVED CORROSION IAW SRM 51-10-05 PAR 15 FIG 5. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG 101 DETAIL IV. L2 DOOR LOWER GATE R & R.SDR CALA2013110800827Cable · out of adjustB757-52-3-007 L1 DOOR FAILED EMERGENCY POWER ACTIVATION CABLE SYSTEM TEST. ADJUSTED L1 DOOR EMERGENCY POWER ACTIVATION CABLE IAW B757-3 AMM 52-11-32-404-010. OPERATIONS CHECKED GOOD.SDR CALA2013110500823Skin · tornSUPPORT TASK FWD CARGO DOOR INNER SKIN TORN AT LOWER MIDDLE LIGHTING HOLE. REPAIRED FWD CARGO DOOR INNER SKIN, LOWER MIDDLE LIGHTING HOLE IAW REO-M0788 & ECRA 5234-01047SDR CALA2013110500817Winglet · damagedSUPPORT TASK LT WINGLET TOP TE CORNER BROKE OFF. REPAIRED LT WINGLET TOP TE CORNER IAW ECRA 5700-03412.SDR CALA2013110500816Winglet · damagedB757-54-3-0348 LIGHTNING STRIKE DAMAGE ON RT WINGLET UPPER AFT CORNER. REPAIRED RT WINGLET UPPER AFT CORNER IAW ECRA 5700- 03413.SDR CALA2013110500814Gate · corrodedCORROSION ON L1 DOOR LOWER GATE EDGE. REMOVED CORROSION IAW SRM 51-10-02 FIG 1. FOUND TO BE OUT OF LIMIT IAW SRM 52-10-02 FIG 101 DETAIL IV. R & R L1 DOOR LOWER GATE ASSEMBLY IAW AMM 52-11-38-004-001 & 52-11-38-404-009.SDR CALA2013110500813Gate · corrodedL2 DOOR HAS CORROSION ON BOTTOM GATE. REMOVED CORROSION IAW SRM 51-10 -02 PAR 15 FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG 101 DETAIL IV. R & R BOTTOM GATE IAW AMM 52-11-38-004-001 & 52-11-38-404-009SDR CALA2013110500807Gate · corrodedCORROSION ON R4 DOOR LOWER GATE EDGE. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02 FIG 101. R & R R4 DOOR LOWER GATE ASSEMBLY IAW SRM 51-40-05 & 51-40-04.SDR CALA2013110500811Seat Track · corrodedSUPPORT TASK CORROSION ON SEAT TRACK AT STATION 680-740 RBL 28. REMOVED CORROSION FROM SEAT TRACK AT BS 680 - 740 RBL 28. ORIGINAL MATERIAL .070 W .046, MATERIAL LOSS .024, MATERIAL REMAINING AREA FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK AT RBL 28 FROM 6SDR CALA2013110500810Shim · corrodedB757-53-3-0526 AFT CARGO BS 1380 RBL 7 FWD SIDE OF FRAME ATTACH SHEAR TIE SHIM HAS CORROSION, NO ALLOWABLE DAMAGE LIMITS FOR SHEAR TIE SHIM PLATE. R & R SHEAR TIE SHIM PLATE AFT CARGO BS 1380 RBL 7 IAW B757- 300 SRM 51-40-02 PAR 4 & 7 FIG 3 & 12.SDR CALA2013110500809Transition Panel · corrodedB757-53-3-0498 FWD CARGO RT SIDE BETWEEN BS 620 & BS 640 RBL 20 TRANSITION PANEL HAS CORROSION SEVERAL PLACES. REMOVED CORROSION FROM FWD CARGO TRANSITION PANEL BETWEEN BS 620 & BS 640 RBL 20. ORIGINAL MATERIAL .063 .011, MATERIAL LOSS .052 & MATERIAL REMAISDR CALA2013102800789Gate · corrodedCORROSION ON L4 DOOR LOWER GATE EDGE. R & R LOWER GATE IAW AMM 52 -11-38-004-001 SUBTASK 034-013.SDR CALA2013102500780Transition Panel · corrodedB757-53-3-0526 AFT CARGO BETWEEN BS 1360 & BS 1380 RBL 20 TRANSITION PANEL HAS CORROSION SEVERAL PLACES. ORIG MATERIAL .063 REMAINING MATERIAL 035 OUT OF LIMITS IAW B757-300 SR M53-00-53 FIG101. REMOVED AFT CARGO PANEL FROM BS1310 TO 1380 & INSTALLED NEW PAN
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