# Service difficulty reports: N152FE A list on [N152FE](https://openairdocs.org/aircraft/N152FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202507211280](https://openairdocs.org/sdr/FDEA202507211280.md): Actuator · failed · Jul 21, 2025 · N152FE · Boeing 7673S2F · Landing Gear Retraction/Extension System > PER FTAM PG 4-31 ALTERNATE LANDING GEAR EXTEND. WHILE ACTIVATING THE ALT GEAR EXTEND SWITCH, THE ALT GEAR FAILED TO EXTEND. FLIGHT TEST LANDING GEAR ALTERNATE SYSTEM WAS TESTED, BOTH TEST WERE SATISFACTORY IAW AMM 32- 32-00-705-001 AND AMM 32-35-00-7 - [SDR FDEA202507081141](https://openairdocs.org/sdr/FDEA202507081141.md): Skin · damaged · Jul 8, 2025 · N152FE · Boeing 7673S2F · Trailing Edge Flaps > DENT ON INBOARD AFT FLAP, INNER SURFACE LH WING INBOARD AFT FLAP, INNER SURFACE LH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 4 DETAIL III NOTE A, SRM 51-70-10-2R REPAIR 4 FIGURE 201 SHEET 1 AND SRM 51-70-03-0G PARAGRAPH 5L FIGURE 16 SHEET 1 - [SDR FDEA202507041119](https://openairdocs.org/sdr/FDEA202507041119.md): Floor Panel · damaged · Jul 4, 2025 · N152FE · Boeing 7673S2F · Fuselage Floor Panel > MDC FLOOR PANEL 251QFF WITH HOLE MDC FLOOR PANEL 251QFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.C REV 92 APR-15-2025 - [SDR FDEA202507041118](https://openairdocs.org/sdr/FDEA202507041118.md): Floor Panel · damaged · Jul 4, 2025 · N152FE · Boeing 7673S2F · Fuselage Floor Panel > MDC FLOOR PANEL 241EFF WITH HOLE MDC FLOOR PANEL 241EFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.C REV 92 APR-15-2025 - [SDR FDEA202507041117](https://openairdocs.org/sdr/FDEA202507041117.md): Floor Panel · damaged · Jul 4, 2025 · N152FE · Boeing 7673S2F · Fuselage Floor Panel > MDC FLOOR PANEL 232NFF WITH HOLE MDC FLOOR PANEL 232NFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.C REV 92 APR-15-2025 - [SDR FDEA202507041116](https://openairdocs.org/sdr/FDEA202507041116.md): Floor Panel · cracked · Jul 4, 2025 · N152FE · Boeing 7673S2F · Fuselage Floor Panel > MDC SECTION 45 FLOOR PANEL 241WFF WITH CRACK MDC SECTION 45 FLOOR PANEL 241WFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.B REV 92.0 APR-15-2025. - [SDR FDEA202507041115](https://openairdocs.org/sdr/FDEA202507041115.md): Floor Panel · cracked · Jul 4, 2025 · N152FE · Boeing 7673S2F · Fuselage Floor Panel > MDC SECTION 45 FLOOR PANEL 241YFF WITH SEVERAL CRACKS MDC SECTION 45 FLOOR PANEL 241YFF, WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.B REV 92.0 APR-15-2025 - [SDR FDEA202403240376](https://openairdocs.org/sdr/FDEA202403240376.md): Rib · damaged · Mar 24, 2024 · N152FE · Boeing 7673S2F · Wing, Rib/Bulkhead > L/H TRI RIB ASSY, 2 EA. DAMAGED HOLES IN RIB 114T2500-5 FROM BOLTS IN STOP BEING SHEARED OFF. **SDR ENTERED IN ERROR** **SDR ENTERED IN ERROR** - [SDR FDEA202307251293](https://openairdocs.org/sdr/FDEA202307251293.md): Skin · gouged · Jul 25, 2023 · N152FE · Boeing 767300 · Fuselage Main, Plate/Skin > GOUGE ON LH FUSELAGE SKIN AT STA 1848.35 AND LBL 9.25 LH UPPER FUSELAGE SKIN AT STA 1848.35 AND LBL 9.25 WAS REPAIRED IAW E-A,#: H-5330- T0375329 - [SDR FDEA202307241283](https://openairdocs.org/sdr/FDEA202307241283.md): Unknown · unknown · Jul 24, 2023 · N152FE · Boeing 767300 · Rudder Structure > RUDDER TRAILING EDGE UPPER TIP WITH LIGHTNING STRIKE. RUDDER TRAILING EDGE UPPER TIP DAMAGE WAS REMOVED IAW B767 SRM 55-40-30-1A FIG.101 NOTE B DETAIL V,X PAG 1-5 REV.86 APR/15/2023. - [SDR FDEA202307191251](https://openairdocs.org/sdr/FDEA202307191251.md): Flap · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Trailing Edge Flaps > LH WING, OUTBOARD FLAP, LOWER SURFACE, NEAR OF OUTBOARD TRACK WITH DENT. LH WING, OUTBOARD FLAP, LOWER SURFACE, WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG.201 SHEET 3 REPAIR 1 AND SRM 51-70-10-2R REPAIR 4 FIG.201 SHEET 2 REV.86 APR 15/23 - [SDR FDEA202307191250](https://openairdocs.org/sdr/FDEA202307191250.md): Floor Panel · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Fuselage Floor Panel > MDC FLOOR PANEL 221DFF WITH DENTS. MDC FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022 - [SDR FDEA202307191249](https://openairdocs.org/sdr/FDEA202307191249.md): Floor Panel · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Fuselage Floor Panel > MDC FLOOR PANEL 222CFF WITH DENTS. MDC FLOOR PANEL 222 CFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022 - [SDR FDEA202307191248](https://openairdocs.org/sdr/FDEA202307191248.md): Floor Panel · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Fuselage Floor Panel > MDC FLOOR PANEL 222AFF WITH DENTS. MDC FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022 - [SDR FDEA202307191247](https://openairdocs.org/sdr/FDEA202307191247.md): Floor Panel · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Fuselage Floor Panel > MDC FLOOR PANEL 222BFF WITH DENTS. MDC FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022 - [SDR FDEA202307191246](https://openairdocs.org/sdr/FDEA202307191246.md): Floor Panel · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Fuselage Floor Panel > MDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022 - [SDR FDEA202307191245](https://openairdocs.org/sdr/FDEA202307191245.md): Floor Panel · dented · Jul 19, 2023 · N152FE · Boeing 767300 · Fuselage Floor Panel > MDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022 - [SDR FDEA202303010358](https://openairdocs.org/sdr/FDEA202303010358.md): Fan · failed · Mar 1, 2023 · N152FE · Boeing 767300 · Air Conditioning System > FWD EQ EXH FAN STATUS MESSAGE DURING CLIMB. CREW DETECTED A BURNING SCENT PRIOR TO THE MESSAGE BUT WENT AWAY IMMEDIATELY AFTER STATUS MESSAGE APPEARED. AMM: 21-58-06 PER FIM 21-58-00 TREE 992 & AM - [SDR FDEA202302160339](https://openairdocs.org/sdr/FDEA202302160339.md): Skin · failed · Feb 16, 2023 · N152FE · Boeing 767300 · Fuselage Main, Plate/Skin > E.A.#:H-5330-T0372987 REPAIR FOR DAMAGE TO FORWARD WING-TO-BODY FAIRING AND SKIN, R/H SIDE, STA 698-720, STR 31-32R. COMPLY WITH E..A. H-5330-T0372987 REV NO: A PS P2 EA H-5330-T0372987 REV NO, P2 WAS SUPERSEDED BY EA H-5330-T0372987 REV A, P2. COMPLIED W - [SDR FDEA202206131425](https://openairdocs.org/sdr/FDEA202206131425.md): Static Inverter · failed · Jun 13, 2022 · N152FE · Boeing 767300 · AC Inverter > DURING EICAS BUS TIE TEST STANDBY INVERTER FAILED TO POWER UP. REPLACED STANDBY INVERTER REF B 767 AMM 24-33-03. - [SDR FDEA202107271876](https://openairdocs.org/sdr/FDEA202107271876.md): Skin · worn · Jul 27, 2021 · N152FE · Boeing 7673S2F · Leading Edge Devices > LH WING. SLAT NO 05 TRAILING EDGE WEDGE WITH TWO WEAR MARKS, LOCATED AT 37 IN FROM INNER RIB AND, 42 IN FROM INNER RIB. LH WING. SLAT NO 05 TRAILING EDGE WEDGE AT POSITION OSS (434.6-447) ON LOWER AND UPPER SKIN WERE REPAIRED I.A.W. SRM 57-43-02-2R FIG. 20 - [SDR FDEA202107271874](https://openairdocs.org/sdr/FDEA202107271874.md): Skin · delaminated · Jul 27, 2021 · N152FE · Boeing 7673S2F · Trailing Edge Flaps > DELAMINATION AT LEFT WING OUTBOARD TRAILING EDGE FLAP, AT 70" FROM INBD TO OUTBD LEADING EDGE. LEFT WING OUTBOARD FLAP, AT 70" FROM INBD TO OUTBD LEADING EDGE WAS REPAIRED I.A.W. SRM 57-53-01-2R PAG. 1-5 TABLE1 FIG. 201 (SHEET 3) AND SRM 51-70-03-0G PAG. 1 - [SDR FDEA202107271875](https://openairdocs.org/sdr/FDEA202107271875.md): Skin · damaged · Jul 27, 2021 · N152FE · Boeing 7673S2F · Leading Edge Devices > RH WING,SLAT #8 BETWEEN LES 446 AND 436, TRAILING EDGE INNER SKIN WITH WEAR. RH WING,SLAT #8 BETWEEN LES 446 AND 436 WAS REPAIRED IAW SRM 57-43-02-2R PAG.1-2 FIG. 201 SHEET 1-2 AND SRM 51-70-10-2R REP. 4 PAG.149-159 FIG.202 SHEET 5 REV 79 DEC 15,2020 - [SDR FDEA201803080636](https://openairdocs.org/sdr/FDEA201803080636.md): Line · leaking · Mar 8, 2018 · N152FE · Boeing 7673S2F · Hydraulic System, Main > DESCENDING THROUGH 13,000 FT, RIGHT HYD QTY AND RIGHT HYD SYS PRESSURE EICAS ILLUMINATED. COMPLIED WITH QRH. LANDED UNEVENTIFULLY. FOUND A LEAK FROM A BROKEN LINE ON THE RT INBD SPOILER ACTUATOR. INSTALLED A NEW UNION ON THE LINE IAW AMM 120-10-09-8- - [SDR FDEA201803080633](https://openairdocs.org/sdr/FDEA201803080633.md): Hydraulic Line · not reported · Mar 8, 2018 · N152FE · Boeing 7673S2F · Hydraulic System, Main > DESCENDING THROUGH 13,000 FT, RIGHT HYD QTY AND RIGHT HYD SYS PRESS EICAS ILLUMINATED. COMPLIED WITH QRH. LAND UNEVENTFULLY INSTALLED RT ACT PRESSURE LINE REF SMP PREFORMED A SUCCESSFUL LEAK CHECK OF BOTH THE RETURN AND PRESSURE LINE. NO LEAKS FOUND. ## 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 = 'N152FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N152FE/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.