N453UP
Service difficulty reports · 415
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 = 'N453UP' 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 = 'N453UP' 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 IPXA2024101541048Bracket · corrodedREMOVED BRACKETS ON STA. 1885.20 2EA. L/H AND 2EA. R/H FOR CORROSION ACCESS ON FRAME. FOUND BRACKETS CORRODED AND CRACKED. INSTALLED 3 EA NEW BRACKETS AND 1EA FABRICATED BRACKET (GUUSSETS) AT STA. 1885.20 IAW B757-200 SRM 51-40-02-0G-0.SDR IPXA2024101240887Strap · corrodedREMOVED AFT LWR. SKIN STRAP AT STA. 1885.20 FOR ACCESS. FOUND CORROSION ON LWR. SKIN STRAP. INSTALLED REPLACEMENT SKIN PLATE ON AFT LOWER FUSELAGE 313AL CUT OUT STA. 1885.20 REF B757 SRM 51-40-02-0G-0. PRODUCTION AUDIT C/WSDR IPXA2024102380040Skin · corrodedLEFT WING OVER WING FILLER CAP HAS CORROSION 52-00. ACCOMPLISHED THE REPAIR PER 757-200PF SRM 57-20-01-2R-6 REPAIR 6 REV 121SDR IPXA2024102314525Skin · corrodedR/H OVER WING FILLER CAP SKIN SHOWS SIGNS OF PITTING ATA 57. ACCOMPLISHED CATEGORY A REPAIR PER 757-200PF SRM 57-20-01-2R-7 (REPAIR 7) REV 121.SDR IPXA2024102994141Web · corrodedSTA. 1681 LBL20 SUB.FLOOR WEB HAS CORROSION AND CRACKED ATA53. ACCOMPLISHED REPAIR PER 757-200PF SRM 53-60-51-2R-6 REPAIR 6 REV 121. REVIEW COMPLETESDR IPXA2024102692207Floorbeam · corrodedDURING WORK ON FAULT T3F18E005847T LINE#843 FOUND CORROSION ON FLOORBEAM LOCATED AT STA 1681 BETWEEN LBL15 AND LBL35. (015-001) ATA53. REVIEWED THE UPS EO FOR ANY DEFERRAL REQUIRMENTS PER EA 757-5310-01-B0294 P4 STEP 20.SDR IPXA2024102232575Floor Support · corrodedMAIN CABIN FLOOR AREA AT STA 1679 HAS FLOOR SUPPORT WITH CORROSION 62INCH FROM BS0 (114-02) ATA 53. REMOVE AND REPLACE RETAINER P/N 146N5064-1 PER DWG 146N5353, DWG 146N5064 AND 757-200PF SRM CHAPTER 51 REV 121 GUIDELINES. UPS CONSIDERS THIS A MINOR REPAIR.SDR IPXA2024100234927Floor Panel · damagedMAIN CABIN FLOOR PANEL 231XJF IS DAMAGED. (114-010) OFF A/C PART ATA 51. ACCOMPLISHED PERMANENT REPAIRS, 3EA CATEGORY A, ON MAIN CABIN FLOOR PANEL 231XJF. REPAIR #1- 24" L X 4" W, LOCATED AT STA 520, 2" FROM O/B EDGE AND 20" FROM AFT EDGE. REPAIR #2- 19.5" L XSDR IPXA2024101768581Strap · corroded[STR] AFT LOWER FUSELAGE. 313AL CUTOUT FWD FRAME LOCATED AT STA 1862.70 HAS CORROSION. (015-17) ATA53. INSTALLED NEW STRAP AT AFT LWR FUSELAGE 313AL CUTOUT FWD FRAME STA. 1862.70 IAW B757-200PF SRM 51-40-02-0G-0. REVIEW COMPLETESDR IPXA2024101568758Skin · corrodedAFT LOWER FUSELAGE. 313AL CUTOUT AFT FRAME LOCATED AT STA 1885.20 HAS CORROSION ON INTERNAL AREA. INSTALLED FAIRING AFT LOWER FUSELAGE STA. 1885.20 / 313AL CUT OUT AFT FRAME, REF. B757-200PF-SRM 51-40-02-0G-0.SDR IPXA2024101170661Door · out of alignmentCREW ENTRY DOOR EXTERNAL SURFACE HAS MISSING PAINT AROUND HANDLE ATA 52. PREPPED AND TOUCHED UP PAINT ON EXTERIOR CREW ENTRY DOOR AROUND HANDLE AREA IAW B757AMM 51-21-10-377-039.SDR IPXA2024091970661Paint · missingCREW ENTRY DOOR EXTERNAL SURFACE HAS MISSING PAINT AROUND HANDLE.SDR IPXA2024053108754Warning Message · illuminated*** EMERGENCY DECLARED *** TE FLAP DISAGREE DURING EXTENSION. USED ALT TO EXTEND FLAPS. TROUBLESHOT TRAILING EDGE FLAP SYSTEM IAW FIM 27-51-808 AND MM 27-51-00-715-001. FLAPS OPERATE NORMAL MULTIPLE TIMES, OK FOR SVC.SDR IPXA2024101206466Skin · delaminatedPANEL ABOVE APU EXHAUST STATION 1941.0-1963.8 HAS DELAM ON INNER SKIN TOP CENTER. (148N3730-47). INSTALLED NEW SKIN ASSY PANEL (P/N 148N3730Y47 BATCH: 0004316631) ABOVE APU EXHAUST STATION 1941.0-1963.8 REF B757-200PF SRM 51-40-02-0G-0 AND DWG: 148N3730. RE-INSDR IPXA2023081951407Unknown · unknownAFT FUSELAGE WHERE MEETS APU EXHAUST HAS CORROSION AND CRACK.***SM100/LMX TO EVAL*** ++ACCOMPLISHED PART REPLACEMENT AS PER SRM 51-40-02 DWG 148N3750SDR IPXA2023081724432Life Raft · unknown01 LIFE RAFT HAS ARMED PIN PULLED OUT. R & R'D LWR LIFE RAFT IAW MM 25-64-00-201.SDR IPXA2022101987285Panel · inoperativeINSPECTION TYPE:N/A**ATB** MCP ALTITUD WINDOW FROZE AT 4900' REMAINDER OF FLIGHT AND AFTER POWER RESET ON GROUND DURING AND AFTER SHUTDOWNR/R'D MODE CONTROL PANEL PER MM 22-11-02-201 PERFORMED MCDP TEST 4 FOR MCP PER FIM22-03-00-815-829 FIG 103 TESTS NORMALSDR IPXA2022080284840Floor Panel · corrodedINSPECTION TYPE:SEG2FLOOR BEAM AT STA 1100 LBL4 HAS CORROSION OUT OF LIMITS. ORIGINAL THICKNESS .200" MATERIAL REMAINING .140" MATERIAL LOSS .060"REPLACED SECTION OF UPPER FLANGE FROM RBL 13.0 TO LBL 12.0 PER EO B757-5310-27-A2990SDR IPXA2022080684960Skin · corrodedINSPECTION TYPE:CK14#1 PYLON AFT SKIN INNER DOUBLER HAD 2 LOCATIONS OF CORROSION DAMAGE. THE FWD CORROSION LOCATION IS LOCATED BETWEEN PP STA 153 AND PP STA 160. THE AFT CORROSION LOCATION IS LOCATED BETWEEN PP STA 182.2 AND PP STA 185.35. BOTH LOCATIONS ARE OSDR IPXA2022072984678Frame · damagedINSPECTION TYPE:SEG2DURING ACCOMPLISHMENT OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT STA 1560 BETWEEN S-24R AND S-27R. ALTERNATE INSPECTION REQUIREDACCOMPLISHED REPAIR PER EO B757-5310-83923-A, UPS RCD 277195 AND VT MAE 757-5360-27-A2984SDR IPXA2022080584952Skin Panel · dentedINSPECTION TYPE:CK14DEFERRAL ITEM# 762227. FUSELAGE SKIN DOUBLER HAS DENT AT STA 400-405 BETWEEN S3L AND S4LREPLACED EXISTING DOUBLER IAW UPS EO B757-5330-45385-C AND VT MAE EA 757-5310-27-A2993SDR IPXA2022052082270Relay · inoperativeINSPECTION TYPE:NAL ENG IDLE IS HIGHER THAN R ENG IN GND, FLT IDLE AS WELL AS WHEN SPOOLING UP. ALL ENG PARAMETERS EPR/EGT/N2/N3/FF SHOW HIGHER DURING GND/FLT IDLE & SPOOL UP NOTE: BLEED AIR DUCT PSI HAS SIGNIFICANT DIFFERENCE, BOTH PACKS.R&R L ENG IDLE CONTROSDR IPXA2021062470914Engine · failedIFSD EMERGENCY DECLARED A/C LANDED WITHOUT INCIDENT A/C OOS** AT 8000 FT LEFT ENGINE FAILED W/NO N3- SHUT DOWN LEFT ENGINE PER QRH.T/S FIM 71-05-00-815-807-R00 STEPS 11-23 & 73-21-00-815-811-R00 STEPS 8-22. R/R'D LH ENG PER TC5001RR & TC5002RR.SDR IPXA2020111362321Tube · leakingINSPECTION TYPE: NA DIVERSION, AC OOS. EMERGENCY DECLARED, NO EMERGENCY EQUIPMENT USED. IN CLIMB & WHEN LEVEL AT FL350 HAD ENGINE INDICATIONS: LT ENGINE EPR 1.73, N1 96.5, EGT 669, N2 89, N3 89, FF 7.0; RT ENGINE EPR 1.71, N1 690, EGT 460, N2 72, N3 77, FF 2SDR IPXA2020111062221Engine · bird ingestionINSPECTION TYPE: NA ATB IFSD. EMERGENCY DECLARED, A/C LANDED W/OUT INCIDENT. LEFT ENGINE LOSS ON ROTATION, BIRD STRIKE, MULTIPLE BIRDS. LEFT ENGINE SHUT DOWN INFLIGHT. C/W BIRDSTRIKE INSPECTION, IAW AMM 05-51-18-212-001, REF LOGBOOK 590403 / 3 FOR R&R OF NSDR IPXA2020090239714Skin · gougedINSPECTION TYPE: SEG #1 PYLON OB SKIN ROUND ACCESS CUTOUT HAS GOUGE. REPAIRED PER EO B757-5430-77663-A.SDR IPXA2020082859590Skin · delaminatedINSPECTION TYPE:SEG, #9 LEADING EDGE SLAT SHOWS DISBOND. REPAIRED SLAT IAW B757 SRM 51-70-10-2R PER SRM 57-43-02-2R-1 SEE E.O. B757-SDR IPXA2020082159282Panel · damagedINSPECTION TYPE:SEG1, RIGHT WING DRY BAY PANEL 632BZ HAS EDGE DAMAGE.REPAIRED PART, DRY BAY PANEL, 632BZ, IAW SRM 51-70-07-OG IAW SRM 57-20-09-2R-1, FIG 201 TABLE I.SDR IPXA2020082159280Panel · damagedINSPECTION TYPE: SEG1, RIGHT WING DRY BAY PANEL 632FZ HAS EDGE DAMAGE. REPAIRED PART, DRY BAY PANEL, 632FZ, IAW SRM 51-70-07-OG IAW SRM 57-20-09-R2-1, FIG 201 TABLE I.SDR IPXA2020041354175Panel · corrodedAPU COMPARTMENT PANEL HAS CORROSION. DRILLED OFF PANEL. FABBED REPAIR DOUBLERS AND FILLER. REMOVED DAMAGE. INSTALLED NEW CORE AND REPAIR PARTS. PRIMED AND PAINTED. REMOVED 9"X2" SECTION OF INNER SKIN AND CORE. FABRICATED INTERNAL DOUBLER FROM 025" 2024T3 & NESDR IPXA2020041354146Support · corrodedINSPECTION TYPE:N/ASUPPORT STRUCTURE UNDERNEATH TAILCONE ON A/C SIDE CORRODEDREPAIRED PER DWG 148N1606 & SRM 51-40-02SDR IPXA2019052342368Pad · missingINSPECTION TYPE:N/A CREW ENTRY DOOR POLY PAD MISSING FROM ENTRY DOOR DAMPER. DEFERRED PER SREO B757-5210-44746-A SUBMITTED REQ 270648A. **SUPPLEMENTAL SDR** R/R CREW ENTRY DOOR DAMPER POLY PAD. OPS CK OK. THIS CLEARS D670765.SDR IPXA2019031340019Hinge Fitting · damagedINSPECTION TYPE:SV NUMBER 1 PYLON IB AFT HINGE FITTING HAS HOLES THAT ARE PAST THE E/O/AD LIMITS. REPAIR OVERSIZED HOLES IAW EA 757-5430-27-A2332 REPLACE #1 TRIB AFT TR MOUNT.SDR IPXA2017080220059Fseu · malfunctionedR & R FSEV NR 1 DUE TO LE SLAT DISAGREE. COMPLIED WITH FIM 27-81-00-815-803. NO FAULTS. R & R FSEU NR 1 IAW MM 27-51-01/201 AND OPS CHECKED IAW MM 27-81-00-715-001. CHECKED GOOD.SDR IPXA2017062318534Warning Message · false activationLE SLAT DISAGREE ON FINAL. TROUBLESHOT IAW FIM 27-81-00, FIG 107, BLOCKS 1-24, WITH NO FAULTS FOUND. ACFT IS OK FOR SERVICE.SDR IPXA2016112811108Warning System · false activationEMERGENCY DECLARED, CREW RECEIVED L/E FLAP DISAGREE EICAS MSG. PERFORMED QRH PROCEDURES. LANDED WITHOUT INCIDENT. PERFORMED LE FLAP SYSTEM AND OPERATIONAL TEST IAW FIM TASK 27-81-00-815-803. NOT FAULT NOTED. OPS CHECK NORMAL.SDR IPXA2016111410596Slat System · malfunctionedL/E SLAT DISAGREE. ACCOMPLISHED QRH CHECKLIST AND LANDED FLAPS 20. TROUBLESHOT IAW FIM, NO FAULTS FOUND. SYSTEM OPERATES NORMALLY IAW FIM 27-81-00-815-803. EMERGENCY DECLARED.SDR IPXA2016102609937Lens · brokenINSPECTION TYPE: UNARMED EMERGENCY LT INDICATOR SWITCH BROKEN. INSTALLED A NEW UNARMED LENS IAW M 33-16-02 & TESTED IAW MM 33-51-00 OPS CHECKED OK.SDR IPXA2016081006848Floor Panel · damagedINSPECTION TYPE: SEG3, MCD FLOOR PANEL 231XWF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016080906842Floor Panel · damagedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XTF HAS EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016072606368Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN CABIN AT BS 560 FLOOR PANEL 232XGF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016072306174Floor Panel · damagedINSPECTION TYPE: C, MAIN CABIN BS 720 FLOOR PANEL 213XPF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016072306168Floor Panel · damagedINSPECTION TYPE:C, MAIN CABIN BS 1100 FLOOR PANEL 242XKF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016080506677Floor Panel · delaminatedINSPECTION TYPE: SEG 3, MCD FLOOR PANEL 252XUF DAMAGED. FABRICATED PANEL 252XUF FROM A402H-48X144, BATTERY 2852496 IAW SREO B757-5320-9692-H.SDR IPXA2016080506675Floor Panel · damagedINSPECTION TYPE: SEG 3, MCD FLOOR PANEL 251XRF DAMAGED. FABRICATED PANEL FROM A402H-48X144, BATTERY 2852496 IAW SREO B757-5320-9692-H.SDR IPXA2016073106505Floor Panel · damagedINSPECTION TYPE: CM, FLOOR PANEL 231XMF DAMAGED. FABRICATED THE FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016072306177Floor Panel · damagedINSPECTION TYPE: C, MAIN CABIN FLOOR PANEL 232XSF DAMAGED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.SDR IPXA2016080806752Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN CABIN AT STA 560 FLOOR PANEL 231XJF DELAMINATED. FABRICATED PANEL 231XKF FROM A402H-48X144 IAW SREO 5320-9692-H.SDR IPXA2016080706712Floor Panel · delaminatedINSPECTION TYPE: C, MAIN CABIN AT STA 560, PANEL 232XJF DELAMINATED. FABRICATED PANEL 232XJF FROM A402H-48X144, BAT 2852496 AND IAW SREO 5320-9692-H.SDR IPXA2016080506676Floor Panel · delaminatedINSPECTION TYPE: SEG 3, MAIN CABIN AT STA 480 FLOOR PANEL 231XFF DELAMINATED. FABRICATED PANEL 231FF FROM A402H-48X144, BATTERY 2852496 IAW SREO B757-5320-9692-H.
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