N158UP

Service difficulty reports · 166

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 = 'N158UP' 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 IPXA2024040339361Seat Track · corrodedMAIN CABIN SEAT TRACK Y "0" HAS CORROSION AT FR STA 82 15-02 REVIEWED. ACCOMPLISH MAJOR PERMANENT REPAIR PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201B (REV 40). REMOVED CORROSION IN SEAT TRACK IAW A300-600 SRM 51-74-10, CHECKED LIMITS AFTER REWORK MAX MATERIAL Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024032939236Web · crackedMAIN CABIN FLOOR WEB, AT FR 77 RIGHT SIDE HAS A CRACK 15-01 INSTALLED NEW WEB. IAW A300-600 SRM 51-40-21. REVIEWEDMar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024040823808Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 12 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. EMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED NEW REPAIR FLANFeb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040823096Skin · crackedTHE L/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 26 FWD. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGE AT CENTER FLAP RIB 26 BETWEEN STR 2.6 TO STR 2.7 AND FABRICATED NEW REPAIR ANGLE WITH MATERIAL 2024-T3 .056C. TRFeb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040825603Skin · crackedTHE R/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 27 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGE AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066 IN ACCOMPLISH WITH STEP 58 ON EAFeb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040825406Skin · crackedTHE R/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 26 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. ACCOMPLISH PERMANENT REPAIR PER EO-89700-REQ1 AND EA 300-5750-27-A3537.Feb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040825155Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 25 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. TREATED AND PRIMED NEW REPAIR DOUBLER IAW A300-600 SRM 51-21-10. NSTALLED NEW DOUBLER IN ACCOMPLISH WITH STED 69 ON EA 300-5750-27-A353Feb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040824763Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 18 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED IAW A300-600 SFeb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040824243Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 17 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED NEW REPAIR FLAFeb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040824047Skin · crackedHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 13 AFT. ON THE UPPER SURFACE. ACCOMPLISH PERMANENT REPAIR PER EO-89700-REQ1 AND EA 300-5750-27-A3537 REV. -.Feb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040823430Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 11 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. FABRICATED NEW REPAIR FLANGE AND NEW REPAIR STIFFENER WITH MATERIAL 2024-T3 .050C BATCH 0004247654 IN ACCOMPLISH WITH STEP 6 ON EA 300-Feb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024040822772Skin · crackedTHE L/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 26 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGES AT CENTER FLAP RIB 26 BTW STR 2.7 TO REAR SPAR AND FABRICATED 02 EA NEW REPAIR ANGLES WITH MATERIAL 2024-T3 .Feb 29, 2024 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2023050693135Door · inoperativeINSPECTION TYPE:NAL1 DOOR SLIDE WILL NOT ARMRELOCATED GRIT BAR COBER AS PER AMM 25-61-21 OPS CHEK DOOR CLOSE AND LATCH NORMALMay 5, 2023 · N158UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2023031391786Warning Light · inoperativeINSPECTION TYPE:NACREW ENTRY DOOR SLIDE WARNING LIGHT INOP. BUZZER FULLY OPERATIONAL. DEFERRED LIGHT INOP PER A300 MEL 52-73-01-1. THIS IS M-804647. PLACARD INSTALLED.RELAMPED CREW ENTRY DOOR WARNING LIGHT. REF AMM 52-73-11. THIS CLEARS DEFERRAL M804647. PLACAMar 10, 2023 · N158UP · Airbus A300F4622R · Emergency ExitsSDR IPXA2022030279605None · noneINSPECTION TYPE:N/ASTRONG BREAD/YEAST WET SOCK ODOR COMING FROM PACKS IN FLIGHT. NO DE ICE FLUID WAS ON THE AIRCRAFT.REMOVED AND REPLACED L/H AND R/H COALESCER BAGS IN REFERENCE TO A300 AMM 21-51-16. ALL CHECKS GOOD.Mar 1, 2022 · N158UP · Airbus A300F4622R · Air Distribution SystemSDR IPXA2021101074795Shroud · crackedINSPECTION TYPE:A300LH WING SKIN PANEL FWD OF 35 SPOILER HAS APPROX 2-2.5 INCH CRACKACCOMPLISHED SKIN PARTIAL REPLACEMENT REPAIRED PER SRM 57-51-12 PARAGRAPH 4G FIG 207Oct 1, 2021 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2021100774731Support · crackedINSPECTION TYPE:CRH WING T/E UPPER FAIRING SUPPORT ANGLE IS CRACKED. LOCATED RIB 10.REMOVED AND REPLACED ANGLE SUPPORT IAW SRM 51-40-21.Sep 25, 2021 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2021100474583None · crackedINSPECTION TYPE:CCRACKED PLATE AT NO.2 PYLON PANEL SUPPORT STRUCTURE BETWEEN PANEL 422DR AND 424CR UPPER CRNER. DOT NO 17-07REMOVE AND REPLACE PLATE PER SRM 51-40-21Sep 25, 2021 · N158UP · Airbus A300F4622R · Nacelle/Pylon StructureSDR IPXA2021070871428Lamp · inoperativeINSPECTION TYPE:N/AEMERG EXIT SIGN 2 EA LAMPS INOPRELAMPED SYS OPS NORMAL REF MM 33-51-00-PB 0501Jul 7, 2021 · N158UP · Airbus A300F4622R · Emergency LightingSDR IPXA2021060770256Warning Message · false activationON CLIMBOUT GOT "PACK 1 OFF" (ECAM). THEN 'STATUS' INDICATED "WING ANTI-ICE INOP" VERIF MAN/IN-LINE PER MEL PROC. SELECTED ANTI-ICE (WING) ON DUE TO WEATHER. GOT "FAULT-USE ALT MODE" & ECAM BLEED 2 FAILED. RESET BLEED & CAB ALT INCREASED FROM 5000FT TO 6500FT Jun 4, 2021 · N158UP · Airbus A300F4622R · Central WarningSDR IPXA2020120763197Bottle · low pressureSLIDE PACK PRESSURE IN RED. DEFERRED SLIDE PER MEL 52 11 01 4. R & R MAIN ENTRY DOOR EVAC SLIDE. OPERATIONS CHECKS GOOD, IAW AMM 25-61-21-0401. OK FOR SERVICE.Dec 7, 2020 · N158UP · Airbus A300F4622R · Escape SlideSDR IPXA2020090359828Slide · inoperativeCREW REPORTS FWD ENTRY DOOR SLIDE WILL NOT ARM. DEFERRED FWD ENTRY DOOR EMERGENCY SLIDE IAW A300 MEL 52-11-01-4. DMP CW. FOUND GIRT BAR EXTENSION & GIRT BAR MISALIGNED WHEN CLOSED. REALIGNED GIRT BAR IAW AMM 25-61-21-0401, OPS CK NORMAL, PLACARD REMOVED THISep 2, 2020 · N158UP · Airbus A300F4622R · Escape SlideSDR IPXA2020052635674Bottle · low pressureINSPECTION TYPE:N/ACREW MAIN ENTRY DOOR EMERGENCY ASSIST BOTTLE BELOW AVERAGE PSI FOR TEMPERATURESERVICED CREW MAIN ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW A300 MM 52-10-14-0301May 4, 2020 · N158UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2019081215533Floorboard · crackedFLOORBOARD CRACKED AT FR 63 14.5'FABRICATED NEW FLOORBOARD PER EO A300-5320-40552Aug 11, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019072744949Floor Panel · crackedINSPECTION TYPE:N/A FLOOR BOARD CRACKED IN HALF. FABRICATED NEW PANEL PER EO A300-5320-40552-B.Jul 27, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019032040298Doubler · crackedINSPECTION TYPE:C123 CRACK INDICATION FOUND IN HOLE "B" IN RT FR47 LOWER CORNER JUNCTION, AT 9:30 O'CLOCK POSITION, 1.425" TO 1.557" IN FROM LOWER EXTERIOR SURFACE. REPAIRED PER REO-G21842 AND EO #A300-5710-71979-A.Mar 2, 2019 · N158UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2019030839835Attach Bracket · crackedINSPECTION TYPE:12YR AFT CARGO COMPARTMENT FORWARD END WALL PANEL ATTACH BRACKET IS CRACKED AT FR-54, RBL-77. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.Mar 2, 2019 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019030839834Attach Bracket · crackedINSPECTION TYPE:12YR AFT CARGO COMPARTMENT FORWARD END WALL PANEL ATTACH BRACKET IS CRACKED AT FR-54, RBL-39. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.Mar 2, 2019 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019030839833Attach Bracket · crackedINSPECTION TYPE:12YR AFT CARGO COMPARTMENT FORWARD END WALL PANEL ATTACH BRACKET IS CRACKED AT FR-54, LBL-39. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.Mar 2, 2019 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019030839832Bracket · crackedINSPECTION TYPE:12YR AFT CARGO COMPARTMENT FORWARD END WALL PANEL ATTACH BRACKET IS CRACKED AT FR-54, LBL-77. REMOVED AND REPALCED BRACKET IAW SRM 51-40-21.Mar 2, 2019 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019052342409Floorboard · damagedINSPECTION TYPE:1C2C MAIN CABIN FLOORBOARD 231QG DAMAGED. REPAIRED PER SREO# A300-5320-42721-F.Feb 27, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019031640121Door Frame · crackedINSPECTION TYPE:12Y AFT CARGO DOOR FRAME FR64 HOLE NR 5 CRACK INDICATION ON FITTING LAYER AT APPROX. THE 9, 12 AND 2 O'CLOCK POSITIONS. REMOVED AND REPLACED FRAME FORK AT FR 64 IAW EO A300-5230-57988-E.Feb 27, 2019 · N158UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2019031640120Door Frame · crackedINSPECTION TYPE:12Y AFT CARGO DOOR FRAME FR63A HOLE NR 5 SHOWS CRACK INDICATION IN FITTING LAYER AT APPROX. THE 12 AND 3 O'CLOCK POSITIONS. REMOVED AND REPLACED FRAME FROK AT FR 63A IAW EO A300-5230-57988-E.Feb 27, 2019 · N158UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2019031239968Floorboard · crackedINSPECTION TYPE:C123 MAIN CABIN FLOORBOARD 242EF DAMAGED. REPAIRED PER SREO A300-5320-42721-F.Feb 27, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019052342411Floor Panel · crackedINSPECTION TYPE:1C2C(PARTS RACK) AFT CARGO COMPARTMENT FLOOR PANEL 151F IS BROKEN. REPAIRED PER EO# A300-5320-16407.Feb 25, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019031640106Floor Panel · crackedINSPECTION TYPE:12Y FORWARD CARGO COMPARTMENT FLOOR PANEL 132PG IS CRACKED. FABRICATED NEW PANEL.Feb 25, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019031640105Floor Panel · crackedINSPECTION TYPE:12Y FORWARD CARGO COMPARTMENT FLOOR PANEL 132MG IS CRACKED. FABRICATED NEW PANEL.Feb 25, 2019 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019030539739Shear Plate · crackedINSPECTION TYPE:123C MAIN CABIN FR79 LT SHEAR PLATE CRACKED. REPAIRED PER EO# A300-5310-58168-A.Feb 22, 2019 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019030539738Shear Plate · crackedINSPECTION TYPE:123C MAIN CABIN FR79 RT SHEAR PLATE CRACKED. REPAIRED PER EO #A300-5310-58168-A.Feb 22, 2019 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019030739816Skin Panel · dentedINSPECTION TYPE:12YR FUSELAGE SKIN DENT BETWEEN FR21-22, STR 53R-54R. REPAIRED IAW SRM 53-10-12, PARA. 10.Feb 20, 2019 · N158UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2018120736670Door · malfunctionedAFTER TAKEOFF AND PUTTING THE LANDING GEAR HANDLE UP, LANDING GEAR RETRACTED. WHEN PLACING THE LG HANDLE TO THE OFF POSITION, RECEIVED AN ECAM FOR L/G DOORS NOT CLOSED. HAD ASSOCIATED LOUD NOISE WITH THE INDICATION. NLG DOOR AMBER LIGHT ILLUMINATED. COMPLDec 5, 2018 · N158UP · Airbus A300F4622R · Landing Gear Door Retract SectionSDR IPXA2018090733700Warning System · false activationAT FL 340 IN CRUISE: ECAM DOOR FWD CARGO NOT CLOSED. PRESSURIZATION REMAINED STABLE, FLT CONTINUED AT FL 340. FWD CARGO DOOR VERIFIED CLOSED AND LOCKED. DOOR WARNINGS NOT INDICATED. CKS GOOD PER AMM 52-71-00-0501. NO HISTORY.Sep 6, 2018 · N158UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2018071331628Light · inoperativeEMERGENCY EXIT LIGHT DIDNT ILLUMINATE WITH GEAR SWITCH DOWN. R&R EXIT LIGHT ASSY PER MM 33-51-13. OPS CK GOOD.Jul 13, 2018 · N158UP · Airbus A300F4622R · Emergency LightingSDR IPXA2018060830407Bracket · bentAFT DOOR PANEL 812BR LOWER AFT FASTENER BRACKET BENT. PERFORMED REPAIR PER E.O.A300-5230-68803-A NO OTHER DEFECTS FOUND, BRACKET REQUIRES SHEET METAL TO REPLACE. REPLACED DAMAGED BRACKET IAW SRM 51-40-21.Jun 8, 2018 · N158UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2018032727901Skin · damagedFUSELAGE SKIN DAMAGED FRAMES 84 - 85, STRINGERS 44 - 45L. REPAIRED IAW EO A300-5330-67751-B.Mar 27, 2018 · N158UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2018020626286Light · inoperativeLIGHT ON THE DOOR ARM - DISARM IS INOPERATIVE WHEN BUZZER IS PUSHED. PERFORMED A BITE TEST OF ASPSU IAW 52-73-00-0501, STEP 13, NO FAULTS OPS NORMALFeb 2, 2018 · N158UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2017122824889Warning Message · false activationEMERGENCY DECLARED, DURING CLIMB OUT, RECEIVED A LEFT FWD CABIN DOOR LIGHT INDICATION ECAM MESSAGE. PERFORMED ADJUSTMENT AND TEST OF DOOR WARNING SWITCHES 14WS AND 16WS IAW AMM 52-71-00-05. OPS CHECKED NORMALDec 23, 2017 · N158UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2017122124704Light · inoperativeEVACUATION SLIDE WARNING SYSTEM LIGHT INOPERATIVE AT THE L1 DOOR. PERFORMED BITE TEST OF ASPSU AND OPS TEST OF SLIDE RELEASE WARNING SYS IAW MM 52-73-00-05 OPS CHECKED NORMAL.Dec 20, 2017 · N158UP · Airbus A300F4622R · Emergency LightingSDR IPXA2017100222231Power Supply · inoperativeESCAPE SLIDE PTT DOES NOT FLASH, AND HORN SOUNDS. R & R APSU 70WN IAW AMM 52-73-18. OPS CHECKED GOODSep 30, 2017 · N158UP · Airbus A300F4622R · Escape SlideSDR IPXA2017061818339Floor Panel · damagedMCD FLOOR PANEL HAS A 2.6 INCH DIA HOLE. FABRICATED A NEW FLOOR PANEL IAW EO A300-5320-40552-BJun 18, 2017 · N158UP · Airbus A300F4622R · Fuselage Floor Panel
Back to N158UP