N408UP

Service difficulty reports · 254

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 = 'N408UP' 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.

SDR IPXA10558804Intercostal · corrodedINSPECTION TYPE:C2, CORROSION ON UPPER FLANGE OF VERTICAL WEB IN THE FWD CARGO BAY, BS 570 TO BS 560, RBL 20, WL 156, STR 26R. REPLACED IAW SRM 51-40-05, SRM 51-40-02.Feb 26, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558740Support · corrodedINSPECTION TYPE:C2 CORROSION ON LT FLOOR TO SIDEWALL SUPPORT PLATE IN THE FORWARD CARGO BAY, BS 510 TO BS 645, LBL 20, WL 156, STR 26L. BLENDED CORRODED AREAS, FOUND TO BE OUT OF LIMITS. REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 53-30-53-0I-1, EO B757-5310-Feb 26, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558739Support · corrodedINSPECTION TYPE:C2 CORROSION ON LT FLOOR TO SIDEWALL SUPPORT PLATE IN THE FORWARD CARGO BAY, BS 510 TO BS 645, LBL 20, WL 156, STR 26L. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED FLOOR TO SIDEWALL SUPPORT IAW EO NR B757-5310-32833-A, SRM 51-40-05Feb 26, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558738Support · corrodedINSPECTION TYPE:C2 CORROSION ON RT FLOOR TO SIDEWALL SUPPORT PLATE IN THE FORWARD CARGO BAY, BS 765 TO BS 840, RBL 20 WL 156, STR 26R. REPLACED RT FLOOR TO SIDEWALL SUPPORT PLATE IN FORWARD CARGO BAY, BS 765 TO BS 840, RBL 20, WL 156, STR 26R REF SRM 51-40-02Feb 26, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558732Support · corrodedINSPECTION TYPE:C2 CORROSION ON LT FLOOR TO SIDEWALL SUPPORT PLATE IN FWD CARGO BAY BS 645 TO BS 765, LBL 20, WL 156, STR 26L. REMOVED AND REPLACED SUPPORT PLATE (SIDE PANEL) PER SRM 51-40-02-0G, SRM 51-40-05-0G.Feb 26, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558876Skin · delaminatedLT HORIZ STABILIZER LOWER SURFACE PREVIOUS REPAIR LOCATED 46" FROM IB, 10" FROM L/E IS DISBONDED. REPAIRED UPS EO B757-5510-37051-A & ER 10-1804 & SRM 51-70-10 UPS EO NR: B757-5510-37051-A.Feb 25, 2010 · N408UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA10558872Skin Panel · misrepairedINSPECTION TYPE:C2, ACCOMPLISH PERMANENT REPAIR TO FUSELAGE SKIN AT BS 530, STR 26R (EFN 408LGPG1004) REF EO B757-5330-36245, REPAIRED IAW ATS ER 10-1754, 3-15-10.Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA10558861Floorbeam · corrodedINSPECTION TYPE:C2, MAIN CARGO FLOOR UPPER FLOOR SUPPORT HAS CORROSION ON ENTIRE SUPPORT BRACKET AT STA 1024 FROM LBL 1 TO LBL 22 WL 208. FABRICATED FLOOR SUPPORT AND UPPER SKIN COMMON TO FLOOR SUPPORT, ALODINED AND PRIME, INSTALLED REF SRM 51-40-05-0G, SRFeb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA10558860Seat Track · corrodedINSPECTION TYPE:C2, MAIN CARGO UPPER FLOOR NUT PLATES CORRODED AT STA 1200 TO STA 1180 RBL 26 WL 208. R & R SEAT TRACK STA 1180-1320 IAW SRM 51-40-02-0G, SRM 51-40-06.Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA10558859Skin · chafedINSPECTION TYPE:C2, RT WING OTBD MAIN FLAP L/E INBD END CHAFED. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-53-01-1A 1, FIG 101, DETAIL VI, ER 10-1845. EO NR: B757-5750-37029-A.Feb 25, 2010 · N408UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA10558858Skin · gougedINSPECTION TYPE:C2, RT WING OTBD MAIN FLAP L/E BULLNOSE IS GOUGED 5.5" FROM INBD END FROM INBD END. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-53-01-1A 1, FIG 101, DETAIL VI, SRM 51-40-02-0G, ER 10-1845 UPS EO NR: B757-5750-37029-A.Feb 25, 2010 · N408UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA10558857Skin · gougedINSPECTION TYPE:C2, RT WING OTBD MAIN FLAP LE BULLNOSE IS GOUGED 5.5" FROM INBD END DAMAGED, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-53-01-1A 1, FIG 101, DETAIL VI, SRM 51-40-02-0G, ER 10-1845 UPS EO NR: B757-5750-37029-AFeb 25, 2010 · N408UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA10558842Frame · damagedINSPECTION TYPE:C2, MCD INTERNAL HAS MECH DAMAGE ON FRAME AT 2 AREAS BS 487 WL 212 AND 217. R & R DAMAGED DOUBLER IAW SRM 52-30-02-1A, SRM 51-40-02-0G, AMM 52-32-05-4.Feb 25, 2010 · N408UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA10558803Frame · gougedINSPECTION TYPE:C2, MCD HAS MECH DAMAGE ON FRAME AT 3 LOCATIONS BS 530, WL 213, 214, 217. REPAIRED IAW ATS 10-1773 DATED 3-9-10.Feb 25, 2010 · N408UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA10558745Web · damagedINSPECTION TYPE:C2 MCD SUPPORT WEB (DOUBLER) HAS MECHANICAL DAMAGE BS 486 WL 232. REMOVED AND REPLACED DOUBLER PER SRM 51-40-02-0G.Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558743Seat Track · corrodedINSPECTION TYPE:C2 MAIN CARGO UPPER FLOOR NUT PLATES CORRODED AT STA 1200 TO STA 1180 RBL 26 WL 208. REMOVED AND REPLACED SEAT TRACK STA 1180-1320 PER SRM 51-40-02-0G, SRM 51-40-0G.Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA10558742Floorbeam · crackedINSPECTION TYPE:C2 MAIN CARGO FLOOR UPPER FLOOR SUPPORT NUT PLATE RIVETS PULLED APART FROM SUPPORT BRACKET AT STA 1024 RBL 1 TO RBL 22 WL 208. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02-0G.Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA10558737Web · damagedINSPECTION TYPE:C2 MCD HAS MECH DAMAGE ON WEB BS 582 WL 214. BLENDED OUT DAMAGE, FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW WEB IAW SRM 52-30-02, SRM 51-40-02-0G, SRM 52-30-02-1A.Feb 25, 2010 · N408UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA10558736Web · damagedINSPECTION TYPE:C2 MCD HAS MECH DAMAGE ON WEB 518 WL 214. BLENDED OUT DAMAGE, FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW WEB IAW SRM 52-30-02-1A, SRM 52-30-02, SRM 52-40-02-0G.Feb 25, 2010 · N408UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA10558735Floorbeam · corrodedINSPECTION TYPE:C2 MAIN CARGO FLOOR UPPER FLOOR SUPPORT HAS CORRODED NUT PLATES AT STA 1056 LBL 1 TO LBL 22 WL 208. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW FLOOR SUPPORT IAW SRM 53-00-51-1A-1, FIG 101, DETAIL II, SRM 51-40-05-0G, SRM Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA10558727Skin · dentedINSPECTION TYPE:C2 LT HORIZONTAL STABILIZER UPPER SURFACE IS DENTED 40 INCHES FROM INBD, 14 INCHES FR FROM L/E. REPAIRED LT HORIZONTAL STABILIZER UPPER SURFACE 40 INCHES FROM INBD, 14 INCHES FROM L/E IAW SRM 51-70-10-2R-4 REPAIR 4 AND SRM 51-70-10-2R REPAIR GFeb 25, 2010 · N408UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA10558708Support · corrodedINSPECTION TYPE:C2 RT WING FAIRING SUPPORT STRUCTURE AT BS 1060, RBL 11 HAS CORROSION ON LWR CHORD. REPAIRED PER SRM 51-70-12-0G.Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA10558691Floorbeam · corrodedINSPECTION TYPE:C2 MAIN CARGO FLOOR UPPER FLOOR SUPPORT HAS CORROSION ON ENTIRE SUPPORT BRACKET AT STA 1024 FROM LBL 1 TO LBL 22 WL208. FABRICATED FLOOR SUPPORT AND UPPER SKIN COMMON TO FLOOR SUPPORT, ALODINED AND PRIME, INSTALLED REF SRM 51-40-05-0G, SRM 51-Feb 25, 2010 · N408UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA10558697Skin · dentedINSPECTION TYPE:C2 SKIN DENTED AT BS 520, 3 INCHES BELOW STR 24 RT. REPAIR WAS PERFORMED ON CUST CARD NR 841250, PER ATS EO 10-1754.Feb 23, 2010 · N408UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA10558493Structure · damagedLEFT WING NR 3 SLAT DAMAGED. REPAIRED PER EO B757-5750-35415-B.Feb 14, 2010 · N408UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA10558488Skin · dentedNR 5 LE SLAT UPPER SKIN DENTED 7.75 INCH OTBD OF INNER EDGE. REPAIRED IAW EO B757-5750-36659-A.Feb 14, 2010 · N408UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA10558487Skin · dentedNR 5 L/E SLAT WEDE DENTED 43.25 INCH OTBD OF INNER EDGE. REPAIRED PER EO B757-5750-36660A.Feb 14, 2010 · N408UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA10558865Support · corrodedINSPECTION TYPE:C2, WHILE REPLACING RT LOWER INBD FUSE PIN, FOUND CORROSION EMITTING BETWEEN BUSHING AND BUSHING BORE ON FWD TRUNNION BRG SUPPORT FITTING. REMOVED BUSHINGS, MACHINED AND SPOTFACED BORE. FABRICATED AND INSTALLED REPAIR BUSHING IAW EO 10-1824.Jan 3, 2010 · N408UP · Boeing 75724APF · Wing, Landing Gear Attach FittingsSDR IPXA09557915Window · bindingCAPTAINS SLIDING WINDOW HANDLE LOAD AT 22LBS. ADJUSTED UPPER WINDOW TRIM PANEL TO ALLEVIATE BINDING CONDITION OF THE LATCH / UNLATCH INDICATION MECHANISM. WINDOW RIG NOT DISTURBED. OPS CHECK OK. REF MM 56-11-02-5.Nov 10, 2009 · N408UP · Boeing 75724APF · Flight Compartment WindowsSDR UPS08553336Unknown · odorINSPECTION TYPE:N/A EXPERIENCED BRIEF PACK ODOR IN C/P AT CRUISE ALTITUDE. SUSPECT LEFT PACK. PERFORMED TROUBLESHOOTING PER FIM 21-00-01 PROCEDURE 2 FOUND NO SYSTEM DEFECTS, OK FOR SERVICE AT THIS TIME.Sep 17, 2008 · N408UP · Boeing 75724APF · Air Distribution SystemSDR UPS06546605Smoke Goggles · crackedSECOND OBSERVERS SMOKE GOGGLES CRACKED. REPLACED SMOKE GOGGLES.Apr 1, 2006 · N408UP · Boeing 75724APF · Emergency EquipmentSDR UPS06547179Frame · dentedINSPECTION TYPE: CK DENT IN FORWARD CARGO FUSELAGE. COMPLIED WITH EA NR 757-5332-27-A1361 AND UPS EO B757-5310-23959-A NO DEVIATIONS NOTED. FINAL CUTOUT.Mar 2, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547178Frame · dentedINSPECTION TYPE: CK DENT IN FORWARD CARGO FUSELAGE. COMPLIED WITH EA NR 757-5310-27-A1354 PRELIMINARY NR 2.Mar 2, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547176Frame · dentedINSPECTION TYPE:CK FORWARD CARGO FUSELAGE FRAME HAS DENT IN STA 740. SEE ECA COMPLIED WITH FINAL EA 757-5322-27-A1357 AND UPS EO NR B757-5310 -24023-AMar 2, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547189Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. SEE ECA. COMPLIED WITH FINAL EA NR 757-5362-27-A1364.Mar 1, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547194Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. COMPLIED WITH FINAL EA NR 757-5362-27-A1369 AND UPS EO NR B757-5310-239 64A - NO DEVIATIONS FROM FINAL EA. NOTE: SEE ECA STEP 18 FOR REPAIR DIMENSIONS.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547193Frame · dentedINSPECTION TYPE:CK DENTS IN AFT CARGO FUSELAGE. REPAIRED DAMAGED AREA IAW EA FINAL 757-5362-27-A1353.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547192Frame · dentedINSPECTION TYPE:CK DENTS IN AFT CARGO FUSELAGE. COMPLIED WITH EA NR FINAL 757-5362-27-A1358 REV.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547191Frame · dentedINSPECTION TYPE:CK AFT CARGO FUSELAGE FRAME HAS DENT. CUT OUT DAMAGE AREA, 1 IN X 1.2 IN X .045 DEEP, OF FRAME PER PRELIMINARY NR 2 EA 757-5362-27-A 1349. HFEC INSPECTION NO CRACKS FOUND IAW WTM PT6 51-00-00. FABBED REPAIR ANGLE IAW NR T61585875, MATERIAL 7Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547190Frame · dentedINSPECTION TYPE:CK DENTS IN AFT CARGO FUSELAGE. COMPLIED WITH EA FINAL B757-5362-27-A1362.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547188Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. COMPLIED WITH FINAL EA NR 757-5362-27-A1347 REV.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547187Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. COMPLIED WITH FINAL EA NR 757-5362-27-A1363 APPLIED CC IAW AMM 25-50-0 0-06.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547186Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. COMPLIED WITH FINAL EA NR 757-5362-27-A1359, AND UPS EO B757-5310-23 960-A. NO DEVIATIONS FROM FINAL EA NOTE: SEE ATTACHED ECA STEP 14 FOR FINAL DIMENSIONS OF (2) EA CUTOUTS AND REPAIR ANGLE.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547185Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. COMPLIED WITH FINAL EA NR 757-5362-27-A1348, AND UPS EO NR B757-5310-23961A. NO DEVIATIONS NOTED. NOTE: SEE STEPS 22 AND 24 ON ATTACHED ECA FOR FINAL DIMENSION.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, StructureSDR UPS06547183Frame · dentedINSPECTION TYPE:CK DENT IN AFT CARGO FUSELAGE. COMPLIED WITH EA NR 757-5362-27-A1366 REV A AND UPS EO NR B757-5310-23 963-B, WITH NO DEVIATIONS FROM EA NOTE: SEE STEPS 16 AND 19 FOR FINAL DIMENSIONS.Feb 28, 2006 · N408UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547182Bulkhead · chafedINSPECTION TYPE:CK NR 1 PYLON AFT BULKHEAD LOWER CORNERS LT & RT SIDE HAVE DEEP CHAFED MARKS ON FOUR LOCATIONS. COMPLIED WITH EA NR 757-5453-27-A1346 HAND UPS EO NR B757-5450-23996-AFeb 28, 2006 · N408UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/FirewallSDR UPS06547181Bulkhead · chafedINSPECTION TYPE:CK NR 2 PYLON AFT BULKHEAD LOWER CORNER AREA LT & RT SIDE HAVE DEEP CHAFFED MARKS. COMPLIED WITH EA NR 757-5453-27 A1346 DATED 3/24/06 AND EO B757-5450-23 23996-A.Feb 28, 2006 · N408UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/FirewallSDR UPS06547290Odor · detectedSTRONG OIL ODOR IN FLT. CAPT & F/O EYE'S & THROAT BURNING. OPERATED LT & RT ENG AT HIGH POWER FOR 15 MIN EA SIDE. ISOLATED LT & RT BLEEDS & APU BLEED. RAN LT & RT PACKS SEPARATELY, NO RE-OCCURRENCE OF OIL ODOR OCCURRED. SYS ODORS CLEAN, NO SMOKE. REF MM Jul 6, 2005 · N408UP · Boeing 75724APF · Air Distribution SystemSDR UPS04543497Latch · brokenINSPECTION TYPE:N/A PILOT REPORT - R2 WINDOW DIFFICULT TO LATCH. CHECKED LATCH HANDLE OPERATION WRT MM 56-11-02-5, OPS OK.Nov 16, 2004 · N408UP · Boeing 75724APF · Flight Compartment WindowsSDR UPS04541960Floor Panel · corrodedINSPECTION TYPE: C, CORROSION ON MAIN DECK FLOOR WEB SURFACE BS 368-375 RBL 22 WL 208. REPAIRED PER SRM 51-70-13.Feb 17, 2004 · N408UP · Boeing 75724APF · Fuselage Floor Panel
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