# Service difficulty reports: N139UP A list on [N139UP](https://openairdocs.org/aircraft/N139UP.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 260 reports - [SDR IPXA20260209570](https://openairdocs.org/sdr/IPXA20260209570.md): Lamp · inoperative · Feb 9, 2026 · N139UP · Airbus A300F4622R · Passenger Compartment Lighting > THREE MDCC LOADING AREA LIGHTS INOPERATIVE. REMOVED AND REPLACED THE THREE LIGHT LAMPS IAW 33-34-41. OPS CHECK GOOD, NO DEFECTS NOTED. - [SDR IPXA2025062734433](https://openairdocs.org/sdr/IPXA2025062734433.md): Sensor · faulted · Jun 26, 2025 · N139UP · Airbus A300F4622R · Engine Bleed Air System > ATB, NR 2 ENGINE BLEED PRECOOLER TEMP 235-VWV 91195430.PERFORMED T/S IAW TSM 36-00-01-0101. REMOVED TEMP CONTROL SENSOR 54HA IAW AMM 36-11-21-0401. RECIVED NEW TEMP CONTROL SENSOR 54HA, VERIFIED EFFECTIVITY IAW A300 IPC 36-11-05-05.INSTALLED SENSOR TEMP CON - [SDR IPXA2025061318214](https://openairdocs.org/sdr/IPXA2025061318214.md): Panel · delaminated · Jun 3, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > WHEEL WELL COMPARTMENT FLOOR PANEL 147EF P/N: A2551027700100 DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO-57698-REQ001 ((APPX B) MAINTENANCE FLOOR PANEL FABRICATION USING ALTERNATE MATERIAL (SREO)) [T3F18E006VAM1]. - [SDR IPXA2025060681128](https://openairdocs.org/sdr/IPXA2025060681128.md): Floor Panel · delaminated · May 31, 2025 · N139UP · Airbus A300F4622R · Fuselage Floor Panel > AFT CARGO FLOOR PANEL 152 SF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO-16407-REQ002 - [SDR IPXA2025060738399](https://openairdocs.org/sdr/IPXA2025060738399.md): Bracket · cracked · May 29, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FR 54 A5341076522300 CRACKED.RECEIVED NEW BRACKET IAW SRM 53-15-18 ITEM 325.LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-40.INSTALLED BRACKET IAW SRM 51-40-21. - [SDR IPXA2025060738376](https://openairdocs.org/sdr/IPXA2025060738376.md): Bracket · cracked · May 29, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FR 54 A5341076522100 CRACKED. INSTALLED NEW BRACKET (1EA) AT FR 54 Y-953 IAW SRM 51-40-21. JOB COMPLETE. REVIEWED - [SDR IPXA2025060738323](https://openairdocs.org/sdr/IPXA2025060738323.md): Frame Angle · cracked · May 29, 2025 · N139UP · Airbus A300F4622R · Fuselage Main, Frame > FR 54/ A5341076521800 ANGLE CRACKED. INSTALLED FR 54/ A5341076521800 ANGLE IAW SRM 51-40-21. - [SDR IPXA2025060594881](https://openairdocs.org/sdr/IPXA2025060594881.md): Intercostal · cracked · May 27, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > UPON FURTHER INVESTIGATION, THIS NON-ROUTINE IS NOT DUPLICATED [T3F18E006LJV7] AND THE EVIDENCE OF THE CRACK IS ON THE INTERCOSTAL, NOT THE FRAME. FR10 Y-953. INSTALLED NEW INTERCOSTAL WEB AT FR10 IAW A300-600 SRM 51-40-21. - [SDR IPXA2025060113072](https://openairdocs.org/sdr/IPXA2025060113072.md): Skin · corroded · May 21, 2025 · N139UP · Airbus A300F4622R · Wing, Plate/Skin > RIGHT WING EXFOLIATION ON T/E UPPER BEAM.INSTALLED FILLER PLATE,DOUBLER AND STATIC DISCHARGER FROM R/H WING TIP IAW SRM 51-40-21 AND SRM57-30-11 FIG 214. - [SDR IPXA2025060188818](https://openairdocs.org/sdr/IPXA2025060188818.md): Seat Track · corroded · May 14, 2025 · N139UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > MDC, FR 27, Y450, SEAT TRACK WITH EXFOLIATION CORROSION. - [SDR IPXA2025053045005](https://openairdocs.org/sdr/IPXA2025053045005.md): Floor Panel · broken · May 7, 2025 · N139UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO, RH SIDE, FLOOR PANEL 132PG IS BROKEN. FABRICATED NEW FLOOR PANEL IAW SREO-16407-REQ002. - [SDR IPXA2025053045015](https://openairdocs.org/sdr/IPXA2025053045015.md): Floor Panel · damaged · May 7, 2025 · N139UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO, RH SIDE, FLOOR PANEL 132SG HAS EDGE DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO-16407-REQ002. - [SDR IPXA2025052965083](https://openairdocs.org/sdr/IPXA2025052965083.md): Web · cracked · May 7, 2025 · N139UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure > #2 ENG PYLON, PRESSURE RELIEF DOOR 423AL, AFT WEB, RIB 3A HAS CRACKS. DOT 103-13A. INSTALLED AFT WEB IAW A300-600 SRM 51-40-21 AND APPLIED TORQUE (T96866) IAW A300-600 AMM 20-21-12/001. REQUEST OK TO INSTALL PRESSURE RELIEF DOOR 423AL. - [SDR IPXA2025060741751](https://openairdocs.org/sdr/IPXA2025060741751.md): Spar · cracked · May 6, 2025 · N139UP · Airbus A300F4622R · Wing Spar > CRACK FOUND IN LOWER HOLE OF FR40 LH LOWER JUNCTION FASTENERS. PERFORMED ROTOTEST IAW NTM 51-10-18 PT 6 PER STEP 31 OF EA# 300-5710-27-A3938. DAMAGE INDICATION FOUND IN FRONT SPAR LAYER. T91112 - [SDR IPXA2025053028751](https://openairdocs.org/sdr/IPXA2025053028751.md): Floorboard · damaged · May 6, 2025 · N139UP · Airbus A300F4622R · Fuselage Floor Panel > FWD. PIT FLOOR BOARD #131DE FR.#26 CORNER DAMAGED DARRYL FORD 91102506. FABRICATED NEW FLOOR PANEL IAW SREO-16407-REQ002. - [SDR IPXA2025051535844](https://openairdocs.org/sdr/IPXA2025051535844.md): Floor Panel · broken · May 6, 2025 · N139UP · Airbus A300F4622R · Fuselage Floor Panel > FAULT: INT-200 ZONE- MAIN DECK FLOOR PANEL 242NM IS CRACKED. FABRICATED FLOOR PANEL 242NM IAW A300 SREO-16407-REQ001. REVIEWED - [SDR IPXA2025060715315](https://openairdocs.org/sdr/IPXA2025060715315.md): Skin · dented · May 5, 2025 · N139UP · Airbus A300F4622R · Elevator, Plate/Skin > LEFT ELEVATOR OUTBOARD LEADING EDGE FWD SIDE IS DENTED, NOT ON ADM. DOT AA017. INSTALLED LEFT ELEVATOR O/B LEADING EDGE FWD SIDE IAW A300-600 SRM 51-40-21. - [SDR IPXA2025060719081](https://openairdocs.org/sdr/IPXA2025060719081.md): Skin · dented · May 5, 2025 · N139UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > FUSELAGE SKIN AT LOWER RIGHT SIDE AT FRAME 92-93 HAS THREE PROTUDING DENTS. NOT ON ADM. DOT AA024 VERIFIED EA 300-5319-27-A3965 PRELIMINARY 2 STEP #9 C/W
VERIFIED SURFACE PROTECTION RESTORED. NOTE: DAMAGE NEEDS TO BE ADDED TO UPS MAPPING. - [SDR IPXA2025060710308](https://openairdocs.org/sdr/IPXA2025060710308.md): Vane · cracked · May 5, 2025 · N139UP · Airbus A300F4622R · Leading Edge Devices > R/H KRUEGER, MOVABLE VANE WITH CRACK UNDER TEFLON ROLLER. VERIFIED STEP# 7, PARTIAL INSTALLATION STEP 2.D.1 (F). - [SDR IPXA2025052697186](https://openairdocs.org/sdr/IPXA2025052697186.md): Adapter · corroded · May 4, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT-STR-Z200-MDC CLS ADAPTER Y 0 AND C28 HAVE CORROSION DOT 07-110 ACCOMPLISHED E.A#: 300-5314-27-A3943 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052697173](https://openairdocs.org/sdr/IPXA2025052697173.md): Adapter · corroded · May 4, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT-STR-Z200-MDC CLS ADAPTER IN Y0 AND C31 HAVE CORROSION DOT 07-109 ACCOMPLISHED E.A#: 300-5314-27-A3944 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052697142](https://openairdocs.org/sdr/IPXA2025052697142.md): Adapter · corroded · May 4, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT-STR-Z200-MDC CLS ADAPTER IN Y0 AND C33 HAVE CORROSION DOT 07-107 ACCOMPLISHED E.A#: 300-5314-27-A3945 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025060885179](https://openairdocs.org/sdr/IPXA2025060885179.md): Skin · delaminated · May 3, 2025 · N139UP · Airbus A300F4622R · Wing, Plate/Skin > LEFT WING OUTBOARD TRAILING EDGE HAS MULTIPLE AREAS OF DELAMINATION AND CORROSION. RECEIVED NEW SECTION PANEL,TRAILING EDGE P/N:A5724701724500 BTCH#:0004400445. INSTALLED NEW SECTION PANEL,TRAILING EDGE FROM L/H WING T/E USED RIVETS (45EA) P/N:CR3212-4-05 BT - [SDR IPXA2025052891073](https://openairdocs.org/sdr/IPXA2025052891073.md): Fitting · cracked · May 3, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FLOOR FRAME ATTACH ANGLE DIRECTLY ABOVE AND TO THE RIGHT OF THE FWD AVIONICS ACCSESS DOOR IS CRACKED. INSTALLED ANGLE AT AVIONIC ACCSESS DOOR IAW WHIT A300-600 SRM 51-40-21. - [SDR IPXA2025052691708](https://openairdocs.org/sdr/IPXA2025052691708.md): Adapter · corroded · May 3, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT-STR-Z200-MDC CLS IN Y 0 AND C36 HAVE CORROSION DOT 07-103 ACCOMPLISHED E.A#: 300-5314-27-A3947 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052691663](https://openairdocs.org/sdr/IPXA2025052691663.md): Adapter · corroded · May 3, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT-STR-Z200-CLS ADAPTER IN Y 0 AND C35 WITH CORROSION DOT 07-104 ACCOMPLISHED E.A#: 300-5314-27-A3946 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052091073](https://openairdocs.org/sdr/IPXA2025052091073.md): Attach Angle · cracked · May 3, 2025 · N139UP · Airbus A300F4622R · Fuselage Main, Attach Fittings > **SDR FILED OPEN**AF-FAULT-STR- FLOOR FRAME ATTACH ANGLE DIRECTLY ABOVE AND TO THE RIGHT OF THE FWD AVIONICS ACCSESS DOOR IS CRACKED VERIFIED STEP #8 GIVEN OK TO INSTALL NEW
ANGLE - [SDR IPXA2025060777381](https://openairdocs.org/sdr/IPXA2025060777381.md): Fitting · cracked · May 2, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > LH HORIZONTAL JUNCTION AREA OF THE CWB LWR ANGLE FITTING AT FR47, CRACK INDICATION NOTED IN HOLE D AT 9 O' CLOCK. VERIFIED REPAIR WAS ACCOMPLISHED BY EO-94114-REQ1 AND EA 300-5710-27-A3940 REV. -. - [SDR IPXA2025061556190](https://openairdocs.org/sdr/IPXA2025061556190.md): Adapter · corroded · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FR 57.1, Y0 L/H SIDE, CLS ADAPTER WITH EXFOLATION. DOT 73-031 VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW UPS EO-93783-REQ1 AND VT-MAE EA 300-5316-27-A3930 REV. - - [SDR IPXA2025061556183](https://openairdocs.org/sdr/IPXA2025061556183.md): Adapter · corroded · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC, FR 57.2, Y0 L/H SIDE, CLS ADAPTER WITH EXFOLATION. DOT 73-030 VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW UPS EO-93782-REQ1 AND VT-MAE EA 300-5316-27-A3933 REV. -. - [SDR IPXA2025061555553](https://openairdocs.org/sdr/IPXA2025061555553.md): Adapter · corroded · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > -MDC FLOOR STRUCTURE FR59 Y0 RH CLS ADAPTER IS EXFOLIATED. VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW UPS EO-93781-REQ1 AND VT-MAE EA 300-5317-27-A3934 REV. - - [SDR IPXA2025052543807](https://openairdocs.org/sdr/IPXA2025052543807.md): Attach Bracket · cracked · May 1, 2025 · N139UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure > RH HORIZ. STAB. TOP APRON FWD. ATTACH BRACKET CRACKED DOT#58-37 DARRYL FORD 91102506. INSTALLED NEW SUPPORT IAW A300-600 SRM 51-40-21 WITH PIN HI-LOK PROTUDING (15 E/A) P/N: HL10VF6-8 BTCH: 0004358078 AND COLLAR P/N: DAN12-6 BTCH:0004130118. INSTALLED R/H HORI - [SDR IPXA2025052655553](https://openairdocs.org/sdr/IPXA2025052655553.md): Adapter · corroded · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT: STR-Z200-MDC FLOOR STRUCTURE FR59 Y0 RH CLS ADAPTER IS EXFOLIATED. DOT 34-051 ACCOMPLISHED E.A#: 300-5317-27-A3934 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052556175](https://openairdocs.org/sdr/IPXA2025052556175.md): Floor Support · cracked · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC FR 80, -Y2462, UNDER PANEL 262HM, AFT FLOOR STRUCTURE WITH CRACK. DOT 73-025. INSTALLED NEW PROFILE (FLOOR STRUCTURE) WITH P/N:A5398140120100 I.A.W. A300-600 SRM 51-40-21. - [SDR IPXA2025052656190](https://openairdocs.org/sdr/IPXA2025052656190.md): Adapter · corroded · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT - STR - Z200 - MDC, FR 57.1, Y0 L/H SIDE, CLS ADAPTER WITH EXFOLATION. DOT 73-031 ACCOMPLISHED E.A#: 300-5316-27-A3929 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052656183](https://openairdocs.org/sdr/IPXA2025052656183.md): Adapter · corroded · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT - STR - Z200 - MDC, FR 57.2, Y0 L/H SIDE, CLS ADAPTER WITH EXFOLATION. DOT 73-030 ACCOMPLISHED E.A#: 300-5316-27-A3933 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025051455228](https://openairdocs.org/sdr/IPXA2025051455228.md): Window Frame · cracked · May 1, 2025 · N139UP · Airbus A300F4622R · Fuselage Main, Structure > RH FRONT UPPER WINDOW FRAME SECTION CRACK INDICATION NOTED IN FWD I/B HOLE AT 3 O' CLOCK AT UPPER ENTABLATURE LAYER. ROTO PERFORMED ON HOLE. HOLE IS FREE OF DEFECTS AT.218". INSPECTION DONE IAW NTM 51-10-01 T96526 T98461. - [SDR IPXA2025052523691](https://openairdocs.org/sdr/IPXA2025052523691.md): Panel · cracked · Apr 30, 2025 · N139UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin > **SDR FILED OPEN** #1 PYLON LH UNDER SIDE PANEL#413CL CRACK ON LOWER SECTION SEE DOT#58/28 DARRYL FORD 91102506 VERIFIED STOP DRILL - [SDR IPXA2025052536184](https://openairdocs.org/sdr/IPXA2025052536184.md): Floorbeam · cracked · Apr 30, 2025 · N139UP · Airbus A300F4622R · Fuselage Main, Floor Beam > **SDR FILED OPEN** FAULT: STR-Z200-MDC FLOOR STRUCTURE AT FR75 L/SIDE FLOOR SUPPORT ANGLE HAS 2EA CRACKS (MARKED IN RED). DOT 34-043 ACCOMPLISHED STEP #3 PER EA# A300-5327-27-A3950. NO CRACKS NOTED AT THIS TIME. T95867 - [SDR IPXA2025052135660](https://openairdocs.org/sdr/IPXA2025052135660.md): Seat Track · corroded · Apr 30, 2025 · N139UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > FAULT: STR-Z200-MDC FLOOR STRUCTURE BTWN FR 80/79 Y1137.1 SEAT TRACK IS CORRORED. DOT 34-040. NSTALLED NEW SEAT TRACK SECTION STRUCTURE BTWN FR 80/79 Y1137.1 IAW A300-600 SRM 53-10-16 PARAGRAPH 4 FIGURE 201 AND SRM 51-40-21. REVIEWED - [SDR IPXA2025052135768](https://openairdocs.org/sdr/IPXA2025052135768.md): Seat Track · corroded · Apr 30, 2025 · N139UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > FAULT: STR-Z200-MDC FLOOR STRUCTURE BTWN FR 80/79 Y0 SEAT TRACK IS EXFOLIATED. DOT 34-042 INSTALLED NEW SEAT TRACK SECTION STRUCTURE BTWN FR 80/79 Y0. IAW A300-600 SRM 53-10-16 PARAGRAPH 4 FIGURE 201 AND SRM 51-40-21. REVIEWED - [SDR IPXA2025052136153](https://openairdocs.org/sdr/IPXA2025052136153.md): Seat Track · corroded · Apr 30, 2025 · N139UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > **SDR FILED OPEN** FAULT: STR-Z200-MDC FLOOR STRUCTURE BTWN FR76/75 Y0 SEAT TRACK IS EXFOLIATED. DOT 34-046 VERIFIED STEP # 15 - [SDR IPXA2025052517581](https://openairdocs.org/sdr/IPXA2025052517581.md): Rub Strip · cracked · Apr 29, 2025 · N139UP · Airbus A300F4622R · Wing Miscellaneous Structure > **SDR FILED OPEN** 1EA FWD RUBBING STRIP WITH A CRACK AT L/H WING CENTER FLAP UPPER SURFACE. DOT 21-57 APPROVED. - [SDR IPXA2025060695800](https://openairdocs.org/sdr/IPXA2025060695800.md): Panel · cracked · Apr 28, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > COVER FR40 RIB-1/RIB 2 IS CRACKED AT 2 LOCATIONS (MARKED IN RED). DOT 34-022 INSTALLED COVER PANEL AT STR-Z600- FR40 RIB-1/RIB 2 IAW A300-600 SRM 51-40-21. - [SDR IPXA2025053196677](https://openairdocs.org/sdr/IPXA2025053196677.md): Adapter · corroded · Apr 28, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC FLOOR STRUCTURE FR57.3/ Y-0 LH UNDER FLOOR PANEL 251PG HAS A CLS ADAPTER CORRODED. DOT 11-69 VERIFIED E.A#:300-5316-27-A3929 PRELIMINARY #1, STEP 14 - [SDR IPXA2025052696730](https://openairdocs.org/sdr/IPXA2025052696730.md): Adapter · corroded · Apr 28, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT: STR-Z200 MDC FLOOR STRUCTURE FR61 RH Y-0 UNDER FLOOR PANEL 252LM HAS A CLS ADAPTER CORRODED. DOT 11-71 ACCOMPLISHED E.A#: 300-5317-27-A3932 PRELIMIRARY #1, STEP #14
VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA2025052696679](https://openairdocs.org/sdr/IPXA2025052696679.md): Adapter · corroded · Apr 28, 2025 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > **SDR FILED OPEN** FAULT: STR-Z200 MDC FLOOR STRUCTURE FR58/ Y-0 RH UNDER FLOOR PANEL 252LM HAS A CLS ADAPTER CORRODED. DOT 11-70 ACCOMPLISHED E.A#: 300-5316-27-A3931 PRELIMIRARY #1, STEP #14 VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. - [SDR IPXA202507316268](https://openairdocs.org/sdr/IPXA202507316268.md): Rib · cracked · Apr 27, 2025 · N139UP · Airbus A300F4622R · Trailing Edge Flaps > MAJOR REPAIR, CRACK FOUND ON RIB 27 AFT (RH) FLAP, MARKED IN RED VERIFIED ACCOMPLISHED E.A.#: 300-5750-27-A3921, PRELIMINARY 1, STEP# 32: - [SDR IPXA202507316163](https://openairdocs.org/sdr/IPXA202507316163.md): Rib · cracked · Apr 27, 2025 · N139UP · Airbus A300F4622R · Trailing Edge Flaps > MAJOR REPAIR, CRACK FOUND ON RIB 13 AFT (RH) FLAP VERIFIED STEP#33 E.A.#: 300-5750-27-A3921, PRELIMINARY 1 REPAIR IS ACCOMPLISHED - [SDR IPXA202507316270](https://openairdocs.org/sdr/IPXA202507316270.md): Rib · cracked · Apr 27, 2025 · N139UP · Airbus A300F4622R · Trailing Edge Flaps > MAJOR REPAIR, 2 CRACKS FOUND ON RIB 26 AFT (RH) FLAP, MARKED IN RED ACCOMPLISHED E.A.#: 300-5750-27-A3921, PRELIMINARY 1, STEP# 32. Next page: https://openairdocs.org/aircraft/N139UP/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N139UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N139UP/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.