N138UP

Service difficulty reports · 250

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 = 'N138UP' 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 IPXA2026081700279Seal · leakingHOWLING SOUND COMING FROM MAIN CABIN DOOR DURING ENTIRE FLIGHT. CRUISE, CLIMB, DESCENT. R & R L1 DOOR SEAL IAW AMM 52-10-18 UP TO & INCL 2.D.(6). REQUIRES TEST AND LEAK CHECK. C/W REMAINING STEPS OF AMM 52-10-18, TEST GOOD. REF T3F18E009AJ1A FOR LEAK CHECK REQAug 14, 2026 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026041338309Lamp · inoperativeLAV EMERGENCY LIGHT INOP. RELAMPED W/REF TO MM 33-51-21 PB 0401Apr 10, 2026 · N138UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026041037458Lamp · inoperativeLAV EMERGENCY LIGHT INOP. RELAMPED LAVATORY AUXILILART/MIRROR LIGHT IAW AMM 33-51-21/401, OPS CHECK GOOD.Apr 10, 2026 · N138UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026012197113Lamp · inoperativeSMALL SQUARE EMERGENCY EXIT LIGHT IN LAV INOP ON LOW SETTING. REPLACED THE LAMPS IAW AMM 33-51-17/401. OPS CHECKED GOOD.Jan 21, 2026 · N138UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025121067021Door · bindingCREW ENTRY DOOR DIFFICULT TO OPEN AND APPEARS TO BIND IN FANNIE HANDLE DOES NOT STAY UP IN ELEVATED POSITION. UNSURE OF WHERE IT IS CATCHING. INSTALLED L1 DOOR REF AMM 52-11-11/401 UP TO AND 2 F (8).Dec 10, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025111882952Actuator · inoperativeYAW DAMPER KICKED OFF WOULD NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-22/401 OPS AND LEAKS CHECKS GOOD OK FOR SERVICE. ALL WORK ACCOMPLISHED BY ALL CAT 3 QUALIFIED TECH.Nov 15, 2025 · N138UP · Airbus A300F4622R · Auto Flight SystemSDR IPXA2025111782952Actuator · faultedEMERGENCY DECLARED, YAW DAMPER KICKED OFF WOULD NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-22/401 OPS AND LEAKS CHECKS GOOD OK FOR SERVICE. ALL WORK ACCOMPLISHED BY ALL CAT 3 QUALIFIED TECH.Nov 15, 2025 · N138UP · Airbus A300F4622R · Auto Flight SystemSDR IPXA2025120741156Skin · puncturedMAJOR REPAIR, DURING CLEAN UP , PUNCTURED INNER FLAP LOWER SKIN INFO SENT TO ENGINEERING ALL STEPS OF EO-95467-REQ4 COMPLETED. THIS IS A PERMANENT REPAIR. THIS DEFERRAL IS NOW CLOSED.Oct 18, 2025 · N138UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025080215434Fitting · crackedCRACK FOUND AT BASE FITTING FR45, RH SIDE.THIS JOB WAS PERFORMED IAW EO-46789-JIC008. (REPAIR - BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177)) [T3F18E00711GE] STEPS 43 THROUGH 53Jul 14, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080115449Fitting · crackedCRACK FOUND AT BASE FITTING FR46, RIGHT SIDE.ACCOMPLISHED EO-46789-JIC008 REPAIR OF FR46 RH SIDE BASE FITTING COMPLETE.Jul 14, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080115146Fitting · crackedCRACK FOUND AT BASE FITTING FR44, RH SIDE. THIS JOB WAS PERFORMED IAW EO-46789-JIC008, REPAIR - BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177).Jul 14, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081943612Skin · damagedCREW DOOR UPPER INNER SKIN HAS BARE METAL EXPOSED. CLEANED AREA AND RESTORED SURFACE PROTECTION IAW A300-600 SRM 51-21-10, SRM 51-75-10 AND AMM 12-21-11.Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025081941352Door · corroded*** SUPPLEMENTAL SDR *** FAULT: STR-ZONE 831- ALL FASTENERS AROUND CREW DOOR EXTERNAL SURFACE CORRODED. JP-110 REVIEWEDJul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025080637021Support · corrodedFAULT- STR- ZONE 100- AFT CARGO FR 58 RH SLOPE STRUCTURE (P/N F539-71534-006-00) IS CORRODED IN 2EA PLACES. 91148554.REMOVED AFT CARGO FR 58 PROFILE BRACKET P/N F539-71534-006-00 IAW A300-600 SRM 51-40-21.RECEIVED NEW SECTION SUPPORT (01EA)P/N F5397153400600 BJul 9, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080637267Support · corrodedFAULT- STR- ZONE 100- FR 57 LH SLOPE STRUCTURE HAS CORROSION IN 1 PLACED MARKED IN RED. 91148554. REMOVED AFT CARGO FR 57 LH PROFILE BRACKET P/N F539-71534-006-00 IAW A300-600 SRM 51-40-21.RECEIVED NEW SECTION SUPPORT (01EA) P/N F5397153400600 BCH# 0004416282.Jul 9, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080537837Angle · crackedFAULT: STR-ZONE 400-#1 PYLON-INSIDE 475AL O/B SIDE 7TH FRAME FROM FWD SIDE-LOWER PART OF FRAME BROKEN ANGLE-109-VWV-91195430.FAB BROKEN ANGLE LOCATED AND DRILLED IAW A300-600 SRM.APPLIED TREATED AND PRIMER TO NEW ANGLE WITH P/N#ALODINE1132 BTCH#4381945 QTY: 1EJul 9, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025080138044Attach Angle · crackedNR 1 PYLON-INSIDE 475AL 4TH STIFFENER FROM AFT END ON I/B SIDE HAS UPPER ATTACH ANGLE BROKEN-109-VWV-91195430 VERIFIED INSTALLATION OF NEW ANGLE.Jul 9, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon, Attach FittingsSDR IPXA2025071043612Skin · damagedCREW DOOR UPPER INNER SKIN HAS BARE METAL EXPOSED.Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025071041352Fastener · corrodedALL FASTENERS AROUND CREW DOOR EXTERNAL SURFACE CORRODED.Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025081918111Panel · crackedPANEL 831BZ HAS CRACK (.500 IN). 91148554 APPLIED ADHESIVE TO DAMAGE AREA OF PANEL 831BZ. P/N EC3532, B/N 0004408668. CURED AND SANDED. IAW AMM 25-00-00/801 PARA 4 REPAIR A STEP (B). RESTORED PROTECTIVE COATING AT REPAIRED AREA. P/N WS-3-BR227K1Q, B/N 00043190Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025081918116Panel · crackedPANEL 831AZ HAS CRACK (.600 IN). 91148554 REPAIRED CRACK WITH 08-116, BATCH 4394542. IAW AMM A300-600 52-34-13/801 PARA 4.3.B.4-6. PAINTED REPAIRED AREA WITH .05 OZ OF 16-407, BATCH 4352735. CUP 02-012-176. IAW AMM A300-600 52-34-13/801 PARA 4.3.C.1.Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025081922065Sight Glass · scratchedL-1 CREW DOOR EMERGENCY SLIDE COVER LOOKING GLASS IS SCRATCHED AND UNABLE TO SEE THROUGH INSTALLED CREW DOOR EMERGENCY SLIDE COVER IAW A300 AMM 52-10-13/401.Jul 8, 2025 · N138UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2025080620169Skin · gougedFUSELAGE TAIL LOWER JACK SECTION, REINFORCE DOUBLER HAS MULTIPLE GOUGES (5EA) AND (1EA) DENT. INSTALLED FILLER, DOUBLER AND BALL AT FUSELAGE TAIL LOWER JACK SECTION IAW 53-10-12-201 PARA 13 FIGURE 210 REV 42 AND SRM 51-40-21.Jul 8, 2025 · N138UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025072822969Frame · brokenNUMBER 2 PYLON, INSIDE 485AL OTBD SIDE 5TH FRAME FWD FROM AFT END HAS BROKEN STIFFENER ON LOWER END. CLIP AND FRAME WAS INSTALLED IAW A300/600 SRM 51-40-21.Jul 8, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2025070918111Panel · crackedPANEL 831BZ HAS CRACK (.500 IN).Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025070918116Panel · crackedPANEL 831AZ HAS CRACK (.600 IN).Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025070922065Sight Glass · scratchedL-1 CREW DOOR EMERGENCY SLIDE COVER LOOKING GLASS IS SCRATCHED AND UNABLE TO SEE THROUGHJul 8, 2025 · N138UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2025080607418Floor Support · brokenMDC FLOOR STRUCTURE REINFORCEMENT SUPPORT CRACKED BTWN FR 38 AND FR 38.1 AT -Y2127.5. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-21 WITH FASTENERS AND SEALANT.Jul 7, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080106493Roller · gougedAFT CARGO COMPT ROLLER @ FRAME 57 LBL 30 DAMAGED. REMOVED AND REPLACED ROLLER BRAKING IAW AMM 25-58-34/0401.VERIFIED 1 EACH ROLLER REMOVED AND REPLACED. JOB COMPLETE.Jul 7, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025071607273Floor Panel · brokenMAJOR REPAIR, MDC FLOOR PANEL 231QH WITH CORNER BROKEN FABRICATED FLOOR PANEL 231QH IAW A300 SREO-16407-REQ001. PAINTED IAW AMM 25-00-00/801.Jul 7, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025073189108Fire Seal · crackedRIGHT PYLON, LOWER MIDDLE FIRE SEAL HAS A CRACK. REMOVED AND REPLACED LOWER FIRE SEAL, IAW SRM 51-40-21.Jul 6, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2025072388961Fitting · crackedLEFT HAND HORIZONTAL JUCTION AREA AT FRAME 47 HOLE #A HAS CRACK AND DAMAGE INDICATIONS IN THE ALL LAYERS IN THE 9 O`CLOCK POSTION FACEING FORWARD. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW EO-94545-REQ1 AND EA 300-5710-27-A4027 REV. -.Jul 6, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025071588161Floor Panel · damagedMAIN DECK FLOOR PANEL 231NG IS DAMAGED. FABRICATED FLOOR PANEL 231NG IAW A300 SREO-16407-REQ001, VERIFIED FABRICATION AND PAINT.Jul 6, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025081278063Floor Panel · damagedFWD CARGO CMPT, FLOOR PANEL 132MG; FR 27-32 RH IS DAMAGED. FABRICATED FLOOR PANEL 132MG IAW SREO-16407-REQ003 STEPS 1 - 19 .Jul 5, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025081278133Floor Panel · damagedFWD CARGO CMPT, FLOOR PANEL 131MG; FR 27-32 LH IS DAMAGED. INSTALLED FABRICATED REPLACEMENT FLOOR PANEL FOR FWD PIT IAW SREO-16407-REQ002 ((APPX C)) JOB COMPLETE. REVIEWEDJul 5, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025072480095Support Bracket · crackedFWD CARGO CMPT FR 38.2; UPPER FLOORBEAM, LOWER CHANNEL SUPPORT BRACKETS (3EA) ARE CRACKED.REMOVED SUPPORT BRACKETS (3EA) AT FRAME 38.2 UPPER FLOOR BEAM IAW A300/600 SRM 51-40-21.FABRICATED NEW BRACKETS (3EA) ON FWD CARGO CMPT FROM MAT. 2024-T3.032C BTCH#:00043Jul 5, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025072970736Seat Track · corrodedMAJOR REPAIR, FLOOR C73 TO C74 AND Y 852 SEAT TRACK WITH EVIDENCE OF CORROSION INSTALLED NEW SEAT TRACK SECCTION ON MDC FLOOR STRUCTURE C71 TO C74 AND Y 852 IAW SRM 53-10-16. RESTORED PROTECTIVE SURFACE ON SEAT TRACK REPAIRED IAW SRM 51 75 10.51 10 16.Jul 4, 2025 · N138UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025072870669Web · crackedMDC FLOOR BETWEEN C73 TO 74 Y2127.5 WEB WITH EVIDENCE OF CRACK IN THE LOWER SURFACE INSTALLED NEW WEB BTW FR73 AND FR74 AT 2127.5 IAW A300-600 SRM 51-40-21.Jul 4, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080750211Adapter · corrodedCORROSION FOUND ON SEAT TRACK (5 LOCATIONS, EACH ONE ON A FRAME) BTW FR21&FR27 -Y65.5 INSTALLED NEW SEAT TRACK ADAPTER, CLS (4E/A) AND NUTPLATES (10E/A) IAW A300-600 SRM 51-40-21.Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025072053158Fitting · crackedCRACK FOUND AT ANGLE-FITTING FR10 Y953 (PN A53612356200) INSTALLED 01 ANGLE FITTING P/N A5361235620000, BCH #0004410795, USING 11 SOLID RIVET IAW SRM 51-40-21 AND SRM 51-21-10Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025071555684Floor Panel · crackedMAIN DECK FLOOR PANEL 232EF IS CRACKED. FABRICATED FLOOR PANEL 232EF IAW SREO-16407-REQ001. PAINTED IAW AMM 25-00-00/801.Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025071655568Floor Panel · brokenMAJOR REPAIR, MAIN DECK CARGO FLOOR PANEL 232WG INSERT IS BROKEN (1 EA) FABRICATED FLOOR PANEL 232WG IAW A300 SREO-16407-REQ001. PAINTED IAW A300 AMM 25-00-00/801.Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025071655508Floor Panel · brokenMAJOR REPAIR. MAIN DECK CARGO FLOOR PANEL 241LM BROKEN FABRICATED FLOOR PANEL 241LM IAW A300 SREO-16407-REQ001.Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025071555422Floor Panel · brokenMAIN DECK FLOOR PANEL 242LJ IS BROKEN. FABRICATED FLOOR PANEL 242LJ IAW A300 SREO-16407-REQ001.Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025071555902Floor Panel · brokenMAIN DECK FLOOR PANEL 231PJ IS DAMAGED AUDIT COMPLETEJul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025071855684Floor Panel · crackedMAIN DECK FLOOR PANEL 232EF IS CRACKED AUDIT COMPLETEJul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025072138048Rib · crackedMAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW EO-94347-REQ1 AND VT-MAE EA 300-5750-27-A4024, REV. -.Jul 2, 2025 · N138UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2025072138064Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 19. CIRCLED IN RED. VERIFIED REPAIR WAS ACCOMPLISHED IAW E0-94347-REQ1 AND EA 300-5750-27-A4024.Jul 2, 2025 · N138UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2025072137992Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. CIRCLED IN RED. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW VT-MAE EA 300-5720-27-A4024 REV- AND EO-94347-REQ1.Jul 2, 2025 · N138UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2025071230622Adapter · corrodedFOUND CORROSION AT CLS ADAPTER FR77 -Y1580.5 REMOVE AND REPLACE THE FR 78 CLS ADAPTER (P/N: A53275455204) LOCATED BETWEEN -Y1221.2 AND -Y1580.5 PER AIRBUS DRAWING A53278756 REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTS. UPS CONSIDERS THIS A MINOR REPAJul 2, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
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