N441UP
Service difficulty reports · 145
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 = 'N441UP' 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 = 'N441UP' 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 IPXA2026091381461Skin · puncturedMAJOR REPAIR. LT ELEVATOR UPPER SURFACE HAS A PUNCTURE. ACCOMPLISH REPAIR IAW WET LAYUP 200 DEG F (93 DEG C) CURE 757-200PF SRM REV 125 CHAPTER 51-70-17-0G-0 PARAGRAPH 4.A REPAIR GENERAL USING SRM 55-20-01-2R-1 REPAIR 1. PERFORMED MOISTURE REMOVAL CYCLE IAWSDR IPXA2026091069069Seal Depressor · crackedMCD DOOR FWD SEAL TRACK HAS A CRACK. REMOVED THE CRACK LOWER SEAL DEPRESSOR FROM MAIN CARGO DOOR FWD EDGE IAW SRM 51-40-02. INSTALLED NEW PART IAW B757-200PF SRM 51-40-02-0G.SDR IPXA2026090236478Floor Panel · corrodedAFT CARGO FOOR PANEL 153AF HAS CORROSION. LOCATED & DRILLED NEW FLOOR PANEL 153AF AFT CARGO IAW SRM 51-40-05. TREATES & PRIMED NEW FLOOR PANEL 153AF IAW SRM 51-20-01.SDR IPXA2026090711902Panel · debondedTHE LT FWD TORQUE BOX PANEL HAS 2EA DELAMINATED, DISBONDED AREAS NEAR FSS 245.653 AND FSS 171.39. REMOVED ALL FASTENERS FROM LT FWD TORQUE BOX PANEL, EXCEPT MOST BOTTOM ROW, & BOTTOM AFT ROW, IAW SRM 51-40-02. INSTALLED NEW TORQUE BOX PANEL ON LT FWD IAW SRSDR IPXA2026090916126Strap · corrodedMAJOR REPAIR, APU INLET DOOR AFT STRAP HAD CORROSION. REMOVED OUTER STRAP IAW SRM 51-40-02-0G-0. INSTALLED NEW REPAIR PARTS AT INLET DOOR AFT STRAP IAW SRM 53-80-15-2R-1,REPAIR 1, DETAIL II.SDR IPXA2026083017738Screen · crackedAFT CARGO PANEL 152CZ SCREEN IS CRACKED. REMOVED CRACK SCREEN AND INSTALLED NEW SCREEN IAW AMM 25-50-03-404-003.SDR IPXA2026090305035Angle · brokenRIGHT WING #8 SLAT MAIN TRACK PANELS (2EA) ARE LOOSE. AFTER A MORE DETAILED INSPECTION, 02 LOOSE RIVETS AND 01 BROKEN ANGLE WERE FOUND ON THE PANELS. 02 RIVETS WERE REMOVED AND REPLACED, BROKEN ANGLE REMOVED. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW BRSDR IPXA2026090305799Firewall · crackedNR 1 ENG OTBD T/R INTERNAL TOP METALLIC PLATE IS CRACKED. REMOVED INTERNAL TOP METALLIC PLATE DAMAGED AND REMOVED SEAL RETAINER (FOR ACCESS). #1 ENG O/B T/R. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED INTERNAL TOP METALLIC PLATE AND SEAL RETAINER. IAW B757-2SDR IPXA2026090314351Support Plate · corrodedFLOOR PANEL JOINT SKIN SUPPORT PLATE CORRODED BELOW NUT PLATE BS 1450 BETWEEN STRG 29-28 (BELOW FLOOR). REMOVED SPLICE STRAP BY SEVERELY EXFOLIATED AT AFT CARGO STA 1450 IAW SRM 51-40-02. INSTALLED NEW PART IAW SRM 51-40-02-0G.SDR IPXA2026090314733Strap · corrodedAPU INLET DOOR FWD STRAP HAS CORROSION. REMOVED FWD STRAP CORRODED I.A.W. B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW STRAP ON APU INLET DOOR FWD IAW B757-200PF SRM 51-40-02.SDR IPXA2026090314768Angle · corrodedAPU INLET DOOR FWD UPPER CORNER ANGLE AT BS 1787.45, S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW UPPER CORNER ANGLE APU INLET DOOR FWD UPPER BS 1787.45, S3R IAW SRM 51-40-02.SDR IPXA2026090514834Angle · corrodedAPU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 S-6R HAS CORROSION. REMOVED LOWER CORNER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW LOWER CORNER ON APU INLET DOOR BS 1787.45 S-6R IAW SRM 51-40-02.SDR IPXA2026090516057Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM BS 1787.45 TO 1825.00 S-3R HAS A CORROSION. REMOVED UPPER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW ANGLE UPPER ON APU INLET DOOR BS 1787.45 TO 1825, S3R IAW SRM 51-40-02.SDR IPXA2026091394413Panel · delaminatedFAULT: COMP-ZONE 600-RIGHT WING LE BEHIND #7 SLAT IB END HAS DELAMINATION. REMOVED FIXED PANEL DAMAGED R/WING I.A.W B757-200PF SRM 51-40-02-0G. CLEANED AND EVALUATED, ITEM IS REPAIRABLE. REMOVED DAMAGE AND FABRICATED NEW CORE PLUG. P/N HRH-10-1/8-3.0, B/N 000SDR IPXA2026090494430Skin · crackedRIGHT WING FIXED LEADING EDGE BEHIND THE NR 8 SLAT HAS A CRACK. ACOMPLISHED REPAIR IAW SREO-11855-REQ002.SDR IPXA2026091095169Panel · delaminatedMAJOR REPAIR, THE RT LWR FWD TORQUE BOX PANEL HAS 1EA DELAMINATED & DISBONDED AREA NEAR FSS 137.467. ACCOMPLISH REPAIR IAW SRM REV 125, 51-70-10-2R-2, 250 DEG F CURE USING SRM 51-70-10-2R-0. DAMAGE WAS REMOVED IAW SRM 51-70-10-2R. BONDED REPAIR PARTS IAW SDR IPXA2026082898567Angle · crackedFWD CARGO BAY, BS 560, RT E5 EE RACK ANGLE CRACKED. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G. INSTALLED A NEW PART & FASTENERS IAW SRM 51-40-02-0G.SDR IPXA2026090886672Panel · corrodedMAJOR REPAIR, NR 1 ENGINE INBD INSIDE PANEL 443JL FWD LOWER PYLON SURFACE HAS CORROSION. CUT & REMOVED THE DAMAGE PART OF PYLON SKIN IAW SRM 51-10-02-0G-0. ACCOMPLISHED REPAIR IAW EO-98556-REQ1 AND STE-MAE EA 757-5450-27-A4612, REV-.SDR IPXA2026090787435Bracket · crackedTHS COMPARTMENT, APU PNEUMATIC DUCT LEFT CLIP SUPPORT CRACKED BS 1787.45. INSTALLED 1EA NEW BRACKET IAW SRM 51-40-02-0G-0.SDR IPXA2026082980687Bracket · crackedFAULT-STR-Z400 #2 ENG AFT PYLON, BRACKET UNDER DIAGONAL BRACE IS BROKEN. REMOVED NR 2 ENG AFT PYLON BRACKED UNDER DIAGONAL BRACE IAW 51-40-02. INSTALLED NEW BRACKET FOR NR 2 ENG AFT PYLON UNDER DIAGONAL BRACE AREA IAW SRM 51-40-02-0G.SDR IPXA2026090472486Frame · crackedDEFERRAL. WHILE ACCOMPLISHED A DETAIL INSPECTION OF THE FUSELAGE SUPPORT, FRAME FOUND A 3 INCH LENGTH CRACK AT BS 1060. ACCOMPLISH THE PERMANENT REPAIR PER EO-98554-REQ1 AND STE-MAE EA 757-5340-27-A4611, REV.SDR IPXA2026090576186Bracket · crackedRT. MLG W/W FWD HD MODULE MOUNT SHOWS EVIDENCEOF A CRACK LOWER AREA. REMOVED MLG W/W FWD HD MODULE MOUNT IAW SRM 51-40-02-0G-0. INSTALLED NEW BRACKET (MLG W/W FWD HD MODULE MOUNT), IAW SRM 51-40-02-0G-0.SDR IPXA2026090377136Angle · corrodedFAULT Z-300 STR: APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1825 S-6R HAS CORROSION. REMOVED LOWER ANGLE CORRODED I.A.W. B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW ANGLE LOWER ON APU INLET DOOR STA 1787.45 TO STA 1825 S-6R IAW B757-200PF SRM 51-40-02SDR IPXA2025121779899Fuel Sys · out of balanceFUEL CONFIG EICAS MSG 2.5 HOURS INTO FLIGHT. LEFT TANK 2,000LBS HIGHER THAN RIGHT TANK. AIRCRAFT OK FOR SERVICE PER AMM 28-21-00-702-001. PERFORMED CROSSFEED LEAK CHECK PER AMM 28-22-02. NO LEAKS FOUND. OBSERVED PRESSURE REFUELING AND NO LEAKS FOUND AND NO FSDR IPXA2025100103715Skin · crackedUPON WORKING EO-88069-REQ047 REV1, TASK CARD T3F18E0054EL6, FOUND EVIDENCE OF POSSIBLE CRACK AT HOLE LOCATION NUMBER 10 L/W UPPR SKIN OF #1 ENG. PYLON. ATA-54-00.PERFORMED BLEND-OUT ON CORRODED AREAS LOCATED AT UPPER FACE SURFACES OF INBD AND OUTB DRAG FITTINSDR IPXA2024092772985Plate · damagedLH ELEV O/B LWR SIDE METAL PLATE BULGING AS MARKED. FABRICATED PRIMED AND INSTALLED SPLICE PLATE PER REF DWG N. 183N2007 FROM MAT P/N: SHT-6061T4-.063 BATCH: 0003785803 REF 757-200 51-40-02-0G-0 / 51-40-05-0G-0.SDR IPXA2024092772979Plate · damagedRH ELEV O/B LWR SIDE METAL PLATE BULGING AS MARKED. FABRICATED PRIMED AND INSTALLED SPLICE PLATE PER REF DWG N. 183N2007 FROM MAT P/N: SHT-6061T4-.063 BATCH: 0003785803 REF 757-200 51-40-05-0G-0 / 51-40-02-0G-0SDR IPXA2024092474202Angle · corroded(STR) CORROSION AT FWD LOWER CARGO DOOR. I/B SIDE, LOWER AREA. PM 040-11. LOCATED, DRILLED AND INSTALLED NEW ANGLE AND RIVETS AT FWD LWR CARGO DOOR I/B SIDE LWR AREA FWD PER REF 757-200 SRM 51-40-02-0G-0. REVIEWED.SDR IPXA2024062668347Fairing · crackedDURING PRE DEPARTURE CHECK FOUND #2 ENG NOSE CONE FAIRING CRACKED. REMOVED AND REPLACED NOSE CONE FAIRING WITH REPAIRED UNIT. REF AMM 72-35-01-004-001-R04 AND AMM 70-51-00. NO DEFECTS NOTED AT THIS TIME.SDR IPXA2024062468347Spinner · crackedDURING PRE DEPARTURE CHECK FOUND #2 ENG NOSE CONE FAIRING CRACKED REMOVED AND REPLACED NOSE CONE FAIRING WITH REPAIRED UNIT. REF AMM 72-35-01-004-001-R04 AND AMM 70-51-00. NO DEFECTS NOTED AT THIS TIME.SDR IPXA2023121827186Fuel Tank · out of balanceRIGHT FUEL INDICATION IMBALANCE OF LESS THAN 1100 LBS WITH ALL OTHER INDICATIONS BALANCED. SAME FUEL FLOW C/W OPS CHECK OF LH BY PASS, NO DEFECTS NOTED AMM 28-22-04. C/W FIM TO REPLICATE FUEL MIGRATION. NO FUEL MIGRATION NOTED FROM RIGHT MAIN TANK. REF FIM 28-SDR IPXA2023121527186Unknown · unknown*SDR FILED OPEN* RIGHT FUEL INDICATION IMBALANCE OF LESS THAN 1100 LBS WITH ALL OTHER INDICATIONS BALANCED. SAME FUEL FLOW TROUBLESHOT WITH BOTH WING TANKS IN TRANSFER CONFIG. PUMPS ON, DEFUEL VALVES OPEN, AND REFUEL VALVES OPEN. FUEL MIGRATES TO LEFT TANK AT SDR IPXA2023120188740Valve · leakingRT ENGINE 1000LBS LESS THAN LEFT ENGINE IN ONE HOUR TIME SEE PREVIOUSLY SUSPECTED FUEL LEAK RT WING DEFUEL VALVE R&R. LEAK AND OPS CK GOOD PER MM 28-26-01. NO MIGRATION NOTED AT THIS TIMESDR IPXA2023112703192Fuel Tank · inoperative*SUPPLEMENTAL SDR* RT TANK 1400 LBS LESS THAN LT TANK AFTER 1 HOUR CRUISE FLT. SEE PREVIUOS FUEL WRITEUP. CTR TANK FUEL DID NOT INCREASE. REMOVED AND REPLACED CTR RH TANK DEFUEL VALVE IAW UPS B757-200 AMM 28-26-01. DEFUELING VALVE LEAK AND OPS CK GOOD PER MM 2SDR IPXA2023112203192Unknown · unknown*SDR FILED OPEN* RT TANK 1400 LBS LESS THAN LT TANK AFTER 1 HOUR CRUISE FLT. SEE PREVIUOS FUEL WRITEUP. CTR TANK FUEL DID NOT INCREASESDR IPXA2023112188740Unknown · unknownRT ENGINE 1000LBS LESS THAN LEFT ENGINE IN ONE HOUR TIME SEE PREVIOUSLY SUSPECTED FUEL LEAK TECH SUPPORT REPORTED THAT WHEN THE €ŒFUEL CONFIG€? LIGHT ILLUMINATED THERE WAS 1200 LBS IN THE CENTER TANK AND 1200 LBS MISSING FROM THE RIGHT TANK. ACCOMPLISHED DESDR IPXA2023030391497Fuel Tank · inoperativeINSPECTION TYPE:NAFUEL TANKS STARTED EXACTLY EVEN- 1 HOUR FLIGHT LEFT= 5.2 RIGHT= 4.1 1,200 IMBALANCE- FUEL FLOWS EVEN.TS FUEL MIGRATION TCH RECOMDS R2 LT WING REFUEL VLV & RT WING DEFUEL REQ # 437274 MM 486211 REM & REPL L/W REFUEL VLV REF UPS AMM 28-21-02 ANSDR IPXA2022092686604Transmission · faultedATB AFTER T/O TRAILING EDGE FLAP DISAGREE EICAS & LIGHT WITH FLAP LEVER AT 0 DEGREES AND FLAPS INDICATING1 DEGREE.PERF'D FIM 27-57-0-815-805 & 27-51-00-815-805 FAULTS LEG 0 FLAP DISAGREE LEG 1 LEVER XMT. REPLACED R WING OB TRANS #8 UP TO AND INCL STEP F3. REMOSDR IPXA2022091486254Shear Plate · corrodedINSPECTION TYPE:SEG3, MAIN CABIN STA 1681 RBL 35 CORROSION LOCATED AT AFT SHEAR WEBWORKED PER UPS EO B757-5310-84662-A, UPS RCD 283456 AND VT MAE 757-5360-27-A3017 REV-SDR IPXA2022091486248Floorbeam · corrodedINSPECTION TYPE:SEG3, EXFOLIATION CORROSION ON 1680 FLOOR BEAM FROM RBL 38.0 TO RBL 41.37 LOCATED ON UPPER BEAM FLANGE LOWER SURFACEWORKED PER UPS EO B757-5310-84662-A, UPS RCD 283460 AND VT MAE 757-5360-27-A3017 REV-SDR IPXA2022091486251Floorbeam · corrodedINSPECTION TYPE:SEG3EXFOLIATION CORROSION ON FLOOR BEAM STA 1680, FROM LBL 38.25 TO LBL 41.25, LOCATED ON THE UPPER BEAM FLANGE LOWER SURFACEWORKED PER UPS EO B757-5310-84662-A, UPS RCD 283544 AND VT MAE 757-5360-27-A3017 REV-SDR IPXA2022091486247Floorbeam · corrodedINSPECTION TYPE:SEG3EXFOLIATION CORROSION ON 1680 FLOOR BEAM FROM RBL 38.0 TO RBL 41.37 LOCATED ON UPPER BEAM FLANGE LOWER SURFACEWORKED PER UPS EO B757-5310-84662-A, UPS RCD 283542 AND VT MAE 757-5360-27-A3017 REV-SDR IPXA2022091386212Skin · corrodedINSPECTION TYPE:SEG3, #2 ENG I/B PYLON INTERNAL BETWEEN NAC STA 130.00-136.00 IS SHOWING SIGNS OF CORROSION.REMOVED CORROSION, PERFORMED HFEC INSP, ALL AREAS WITHIN LIMITS IAW SRM 54-50-01-1A-1SDR IPXA2022091386228Web · corrodedINSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT LEFT LOWER FLOOR PANEL AREA UNDER PANEL 221XBF SHOWS EVIDENCE OF CORROSION AT STA 345.BLEND OUT FOUND AT MAIN CABIN TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-10-51-1A-2SDR IPXA2022091286179Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT, UNDER FLOOR PANEL 222XAF HAS AREAS OF CORROSION AT STA 345 CORROSION IS LOCATED ON THE SHEAR WEB BETWEEN STA 332 AND STA 340 RBL 17 TO RBL 24.25AFTER BLENDOUT THE AREA, FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-SDR IPXA2022091286157None · noneINSPECTION TYPE:SEG3DURING ACCOMPLISHMENT OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT STA 1240 R/HACCOMPLISHED REPAIR PER EA 757-5360-27-A3012 REV-SDR IPXA2022091286154Frame · dentedINSPECTION TYPE:SEG3RT FRAME STA 580 BETWEEN S16 AND S17 HAS DENT AT MAIN CARGO COMPARTMENTACCOMPLISHED REPAIR IAW SRM 53-30-07-2R-1 DETAIL VISDR IPXA2022091286153Frame · dentedINSPECTION TYPE:SEG3FRAME STA 660 BETWEEN STA 17 AND STR 16 HAS A DENT AT LOWER AREAACCOMPLISHED REPAIR IAW SRM 53-30-07-2R-1 DETAIL ISDR IPXA2022091086092Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CABIN FLOOR STA 340-368 LBL 25, AROUND HOLES HAS CORROSION. CORROSION LOCATED AT THE SHEAR WEB BETWEEN STA 330.8 AND STA 395 LBL 35.0.AFTER THE BLENDOUT ALL AREAS, SHEAR WEB WAS FOUND TO BE IN LIMITS PER SRM 53-10-51-1A-2.SDR IPXA2022091086099Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CARGO COMPT UNDER FLOOR PANEL 222 XCF HAS AREAS OF CORROSION BETWEEN STA 418 AND STA 440. CORROSION LOCATED AT THE SHEAR WEB BETWEEN STA 398.5 AND STA 431.75 RBL 49AFTER THE BLENDOUT ALL AREAS, SHEAR WEB WAS FOUND TO BE IN LIMITS PER S
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