# Service difficulty reports: Boeing 757-2B7

A list on [Boeing 757-2B7](https://openairdocs.org/model/boeing-757-2b7.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 75 · 3,730 reports

- [SDR FDEA202607110913](https://openairdocs.org/sdr/FDEA202607110913.md): Control Valve · odor · Jul 11, 2026 · N901FD · Boeing 7572B7 · Cabin Cooling System
  > FUME EVENT DESCEND THROUGH 20-25K. IT WAS A DIRTY OILY SOCK SMELL. PERFORMED INSPECTION OF HIGH PRESSURE DUCT & INTERMEDIATE PRESSURE DUCT ON BOTH ENGINES. REMOVED AND REPLACED LEFT WATER EXTRACTOR ASSY LEAK AND OPS CHECK GOOD. REMOVED AND REPLACED LEFT P
- [SDR FDEA202605300654](https://openairdocs.org/sdr/FDEA202605300654.md): Stowage Box · damaged · May 30, 2026 · N903FD · Boeing 7572B7 · Crew Oxygen System
  > WHILE PRE FLIGHTING AC FOUND CAPTS O2 MASK BOX TEST BUTTON BROKEN. REMOVED AND REPLACED CAPTS 02 MASK STOWAGE BOX PER 757 AMM 35-11-51-4-99. OPS CHECK GOOD. MVP COMPLETED BY 4706850 O2 CYLINDER OPENED.
- [SDR FDEA202604250500](https://openairdocs.org/sdr/FDEA202604250500.md): Circuit Breaker · tripped · Apr 25, 2026 · N903FD · Boeing 7572B7 · Fuel System Wiring
  > LEFT AND RIGHT FUEL OVERRIDE CIRCUIT BREAKERS ARE TRIPPED ON PREFLIGHT. REINSTALLED THE P33 PANEL. AWAITING RETEST REQUIREMENTS FROM ENGINEERING IAW AMM: 20-11-00-2 AND SWPM 20-60-03. PANEL P33 INSTALLATION CHECK PER MTSIS AND MOCC.
- [SDR FDEA202602100158](https://openairdocs.org/sdr/FDEA202602100158.md): Skin · cracked · Feb 10, 2026 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Plate/Skin
  > ENG # 1 NACELLE STRUT UPPER WING SURFACE SPAR MID-SPAR ATTACH FITTING HAS A BOLT MIGRATED THIS ITEM HAS BEEN ACCOMPLISHED FOLLOWING WORK INSTRUCTIONS AS PER EA # F-5730- T0386126 P1 TITTLE:"WINGS-PLATES AND SKINS-LH WING UPPER SKIN AT PYLON-LOOSE FASTENE
- [SDR FDEA202602070144](https://openairdocs.org/sdr/FDEA202602070144.md): Wedge · damaged · Feb 7, 2026 · N903FD · Boeing 7572B7 · Leading Edge Devices
  > NUMBER 9 LEADING EDGE SLAT WEDGE DEBONDED, TWO PLACES. APPLIED A PERMANENT REPAIR TO NR 9 LE SLAT EDGE WEDGE IAW SRM 51-70-10-2R R ESTORED SURFACE IN REPAIRED AREA IAW IAW AMM 51-21-00-7.
- [SDR FDEA202602070143](https://openairdocs.org/sdr/FDEA202602070143.md): Wedge · damaged · Feb 7, 2026 · N903FD · Boeing 7572B7 · Leading Edge Devices
  > NUMBER 7 LEADING EDGE SLAT WEDGE DEBONDED. REPAIRED NR 7 LEADING EDGE SLAT IAW SRM 51-70-10-2R.TAP TEST RESULTED SATIFACTORY IAW SRM 51-10-06-2R.
- [SDR FDEA202602040127](https://openairdocs.org/sdr/FDEA202602040127.md): Stringer · damaged · Feb 4, 2026 · N903FD · Boeing 7572B7 · Fuselage Main, Longeron/Stringer
  > REMOVE EXISTING REPAIR AT STA 1656 ON STRINGER 26L REPAIRED STRINGER SECTION AT BS 1640 11" TO BS1660 10" STR 26L, IAW B757 SRM 53-00-03-2R, FIG 201, DETAIL I AND B757 SRM 51-40-02-0G
- [SDR FDEA202601300106](https://openairdocs.org/sdr/FDEA202601300106.md): Floor Support · mechanic error · Jan 30, 2026 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT, BS 1465 MISDRILLED HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT, IAW SRM 51-40-02-0G AND SRM 53-60-53-01, FIG 1, DET VII.
- [SDR FDEA202601300105](https://openairdocs.org/sdr/FDEA202601300105.md): Floor Support · mechanic error · Jan 30, 2026 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT, LBL 7.55 BTW BS 1480 TO 1500 MISDRILLED HOLES REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G AND SRM 53-60-53-0I FIG 1 DET VII
- [SDR FDEA202601280095](https://openairdocs.org/sdr/FDEA202601280095.md): Skin · dented · Jan 28, 2026 · N903FD · Boeing 7572B7 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 TWO DENTS, APPLIED PERMANENT REPAIR AT UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 IAW SRM 53-80-01-1A, FIG 101, SHEET 2, NOTE C, & SRM 51-70-10-2R.
- [SDR FDEA202601190068](https://openairdocs.org/sdr/FDEA202601190068.md): Skin · corroded · Jan 19, 2026 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 134.76 CORRODED. THIS ITEM HAS BEEN ACCOMPLISHED ON EA # F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATES/PANELS- # 2 PYLON O/B SIDE SKIN-EXISTING REPAIR DOUBLER BETWEEN PP STA 174-190, WITH
- [SDR FDEA202601190067](https://openairdocs.org/sdr/FDEA202601190067.md): Skin · corroded · Jan 19, 2026 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 200.50 SUSPECTED CORROSION. ACCOMPLISHED ON EA F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATES/PANELS # 2 PYLON O/B SIDE SKIN-EXISTING REPAIR DOUBLER BETWEEN PP STA 174- 190, WITH CORROSION
- [SDR FDEA202512162256](https://openairdocs.org/sdr/FDEA202512162256.md): Battery Pack · no test · Dec 16, 2025 · N903FD · Boeing 7572B7 · Emergency Lighting
  > L1 EMERGENCY EXIT LIGHT FAILS TO TEST DURING PRE-FLT. REMOVED AND REPLACED THE BATTERY PACK FOR THE L 1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-07-2 EMERGENCY EXIT LIGHT TEST NORMAL. BATTERY PACK RADIANT POWER CORP.
- [SDR FDEA202511212196](https://openairdocs.org/sdr/FDEA202511212196.md): Bulb · failed · Nov 21, 2025 · N901FD · Boeing 7572B7 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2. OPS CHKD SERVICEABLE.
- [SDR 7C7A2025101200043](https://openairdocs.org/sdr/7C7A2025101200043.md): Battery Pack · inoperative · Oct 12, 2025 · N628NP · Boeing 7572B7 · Emergency Lighting
  > FWD GALLEY EMERGENCY LIGHT INOP.
- [SDR 7C7A2025100300042](https://openairdocs.org/sdr/7C7A2025100300042.md): Stop Fitting · gouged · Oct 3, 2025 · N628NP · Boeing 7572B7 · Fuselage Main, Structure
  > L4 DOOR FWD FRAME UPPER STOP FITTING IS GOUGED.
- [SDR 7C7A1900010000041](https://openairdocs.org/sdr/7C7A1900010000041.md): Sleeve · dented · Oct 2, 2025 · N628NP · Boeing 7572B7 · Engine Thrust Reverser
  > NR 2 ENGINE INBD THRUST REVERSER SLEEVE HAS A DENT 18 INCHES FROM TOP EDGE AND 15 INCHES FROM FWD EDGE.
- [SDR 7C7A2025100200040](https://openairdocs.org/sdr/7C7A2025100200040.md): Heat Shield · cracked · Oct 2, 2025 · N628NP · Boeing 7572B7 · Landing Gear Doors
  > LEFT MLG BODY DOOR OUTER SURFACE HEAT SHIELD COVER IS CRACKED AND DELAMINATED.
- [SDR FDEA202509261839](https://openairdocs.org/sdr/FDEA202509261839.md): Actuator · failed · Sep 26, 2025 · N901FD · Boeing 7572B7 · Landing Gear Retraction/Extension System
  > ON TAKE OFF OUT OF MEM, LANDING GEAR WOULD NOT RETRACT. RAN QRH, LANDING GEAR RETRACTED WITH LOCK OVERRIDE. LANDING GEAR EXTENDED NORMALLY ON APPROACH INTO FSD. A/C SHOWED LT TRUCK TILT SENSED IT WAS STILL ON THE GROUND. DISCONNECTED AFT END OF TRUCK TIL
- [SDR FDEA202509261838](https://openairdocs.org/sdr/FDEA202509261838.md): Packing · failed · Sep 26, 2025 · N901FD · Boeing 7572B7 · Landing Gear Retraction/Extension System
  > TAKEOFF ROTATION ON DEPARTURE IN MEM DID NOT FEEL NORMAL. IT FELT LIKE THE GEAR TRUCKS DID NOT TILT. AMM: 32-32-15-4 ON INSPECTION OF LEFT TRUCK TILT ACTUATOR, FOUND THE BLEED PLUG LEAKING FLUID ALLOWING ACTUATOR PISTON TO MOVE FREELY. THE PLUG WAS LOOS
- [SDR 7C7A2025091800039](https://openairdocs.org/sdr/7C7A2025091800039.md): Apu · oil consumption · Sep 18, 2025 · N629NP · Boeing 7572B7 · APU Oil System
  > HIGH OIL CONSUMPTION AUTO SHUTDOWN ACTIVATED
- [SDR FDEA202508261543](https://openairdocs.org/sdr/FDEA202508261543.md): Battery · inoperative · Aug 26, 2025 · N903FD · Boeing 7572B7 · Emergency Lighting
  > DURING MX PRE-FLIGHT FOUND OVERHEAD EMERGENCY LIGHTS AT CENTER, AND R1 DOOR AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE BATTERY FOR OVER AN HOUR, NO FIX. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY (M730) AS PER ABOVE REF. ALL LIGHTS NOW WORKING.
- [SDR 7C7A2025081600038](https://openairdocs.org/sdr/7C7A2025081600038.md): Access Panel · delaminated · Aug 16, 2025 · N627NP · Boeing 7572B7 · Wing, Plate/Skin
  > RIGHT UPPER WING ACCESS PANEL 611KT FOUND DELAMINATED.
- [SDR 7C7A2025081600037](https://openairdocs.org/sdr/7C7A2025081600037.md): Hydraulic Line · gouged · Aug 16, 2025 · N627NP · Boeing 7572B7 · Hydraulic System, Main
  > LEFT NACELLE REVERSE FLOW CHECK CONTROL LINE FOUND GOUGED.
- [SDR 7C7A2025081600036](https://openairdocs.org/sdr/7C7A2025081600036.md): Sign · inoperative · Aug 16, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > AFT GALLLEY RIGHT SIDE EMERGENCY EXIT SIGN INOPERATIVE, WON'T TURN ON.
- [SDR 7C7A2025081600035](https://openairdocs.org/sdr/7C7A2025081600035.md): Sign · inoperative · Aug 16, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > L3 DOOR EXIT IND SIGN INOPERATIVE.
- [SDR 7C7A1900010000034](https://openairdocs.org/sdr/7C7A1900010000034.md): Sign · no test · Aug 16, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC, AND EXIT SIGN INOPERATIVE, NO TEST.
- [SDR 7C7A2025081600033](https://openairdocs.org/sdr/7C7A2025081600033.md): Skin · dented · Aug 16, 2025 · N627NP · Boeing 7572B7 · Leading Edge Devices
  > RIGHT WING NR 6 SLAT TRAILING EDGE UPPER SKIN.
- [SDR 7C7A2025081600032](https://openairdocs.org/sdr/7C7A2025081600032.md): Skin · debonded · Aug 16, 2025 · N627NP · Boeing 7572B7 · Elevator, Plate/Skin
  > RIGHT UPPER SURFACE SKIN PATCH DE-BONDED.
- [SDR 7C7A2025081500031](https://openairdocs.org/sdr/7C7A2025081500031.md): Fairing · damaged · Aug 15, 2025 · N627NP · Boeing 7572B7 · Trailing Edge Flaps
  > EVIDENCE OF DAMAGE AT EDGE OF CANOE PANEL 672HB.
- [SDR 7C7A1900010000030](https://openairdocs.org/sdr/7C7A1900010000030.md): Skin · damaged · Aug 15, 2025 · N627NP · Boeing 7572B7 · Wing, Plate/Skin
  > RIGHT WINGTIP HAS LIGHTING STRIKE.
- [SDR 7C7A1900010000029](https://openairdocs.org/sdr/7C7A1900010000029.md): Skin · dented · Aug 15, 2025 · N627NP · Boeing 7572B7 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN STA 846 BETWEEN S-4L AND S-5L.
- [SDR 7C7A1900010000028](https://openairdocs.org/sdr/7C7A1900010000028.md): Skin · dented · Aug 14, 2025 · N627NP · Boeing 7572B7 · Rudder, Plate/Skin
  > VERTICAL STABILIZER LH LOWER SIDE OF RUDDER HAS DENT
- [SDR 7C7A1900010000027](https://openairdocs.org/sdr/7C7A1900010000027.md): Skin · dented · Aug 14, 2025 · N627NP · Boeing 7572B7 · Fuselage Main, Plate/Skin
  > DENT ON PREVIOUS BLEND ON FUSELAGE SKIN AT STA 481 BETWEEN STR 27L-28-L.
- [SDR 7C7A2025081300026](https://openairdocs.org/sdr/7C7A2025081300026.md): Skin · dented · Aug 13, 2025 · N627NP · Boeing 7572B7 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN STA 1697 BETWEEN S-18L AND S-19L.
- [SDR 7C7A202508130001](https://openairdocs.org/sdr/7C7A202508130001.md): Hinge · damaged · Aug 13, 2025 · N627NP · Boeing 7572B7 · Trailing Edge Flaps
  > LH ENG OB LOWER BLOCKER FLAP #6 FROM 12 OCLOCK POSITION LOWER HINGE ATTACHEMENT PLATE HAS MISSING PIECE
- [SDR 7C7A1900010000024](https://openairdocs.org/sdr/7C7A1900010000024.md): Skin · dented · Aug 13, 2025 · N627NP · Boeing 7572B7 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AT STA 531 BETWEEN STR 28L AND 28R
- [SDR 7C7A1900010000023](https://openairdocs.org/sdr/7C7A1900010000023.md): Battery Pack · no test · Aug 9, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC INOP LIGHT ALONG WITH EXIT SIGN.
- [SDR 7C7A2025080600022](https://openairdocs.org/sdr/7C7A2025080600022.md): Switch · broken · Aug 6, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > DURING INSTALLATING AFT 3 LH DOOR LINNERS FJOUND SLIDE LIGHT INDICATIO SWITCH BROKEN
- [SDR 7C7A1900010000021](https://openairdocs.org/sdr/7C7A1900010000021.md): Light · broken · Aug 2, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > DURING INSTALLING AFT 4 R/H DOOR LINERS FOUND SLIDE LIGHT INDICATOR SWITCH CONNECTOR BROKEN
- [SDR 7C7A1900010000020](https://openairdocs.org/sdr/7C7A1900010000020.md): Battery · discharged · Aug 2, 2025 · N627NP · Boeing 7572B7 · Emergency Lighting
  > EMERGENCY MARKER AT R3 DOOR INOPERATIVE.
- [SDR 7C7A1900010000019](https://openairdocs.org/sdr/7C7A1900010000019.md): Fuse · failed · Aug 2, 2025 · N627NP · Boeing 7572B7 · Light System Wiring
  > AFT GALLEY R/H SIDE EMERGENCY EXIT MAKER INOP
- [SDR FDEA202507201277](https://openairdocs.org/sdr/FDEA202507201277.md): Seat Track · corroded · Jul 20, 2025 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 440 TO BS 640 LBL 24.75 WITH MULTIPLE SPOTS CORRODED UPPER / LOWER FLANGE SURFACE.
- [SDR FDEA202506281076](https://openairdocs.org/sdr/FDEA202506281076.md): Support Beam · corroded · Jun 28, 2025 · N909FD · Boeing 7572B7 · Fuselage Main, Structure
  > CARGO COMPARTMENT SUPPORT BEAM LOWER CHORD BS 1360 BETWEEN RBL 24.75 AND RBL 45.50 NUTS PLATE WITH CORROSION.
- [SDR FDEA202506281075](https://openairdocs.org/sdr/FDEA202506281075.md): Shear Tie · corroded · Jun 28, 2025 · N909FD · Boeing 7572B7 · Fuselage Internal Mounting Structure
  > AFT CARGO MCOMPARTMENT SHEAR TIE CORRODED AT BS 1480 BETWEEN STRINGER 28R - STR29R.
- [SDR FDEA202506281074](https://openairdocs.org/sdr/FDEA202506281074.md): Shear Tie · corroded · Jun 28, 2025 · N509FD · Boeing 7572B7 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 1500 BETWEEN STR 28R - STR 29R.
- [SDR FDEA202506271067](https://openairdocs.org/sdr/FDEA202506271067.md): Support · corroded · Jun 27, 2025 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CEILING SUPPORT HAS CORROSION BETWEEN BS 1400.0 TO BS 1420.0 RBL 24.75.
- [SDR FDEA202506271066](https://openairdocs.org/sdr/FDEA202506271066.md): Support · corroded · Jun 27, 2025 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CEILING PANEL SUPPORT HAS CORROSION BETWEEN BS 1400.0 TO BS 1420 RBL 45.50.
- [SDR FDEA202506261063](https://openairdocs.org/sdr/FDEA202506261063.md): Floorbeam · corroded · Jun 26, 2025 · N909FD · Boeing 7572B7 · Fuselage Main, Floor Beam
  > MCC FLOOR BEAM SUPPORT UPPER HAS CORROSION RBL 8 -14 STA 560. PERFORMED FLOOR BEAM REPAIR AT MCC STA 560 FROM RBL 15.8 TO LBL 11.1 ON UPPER CHORD IAW B 757 SRM 53-00-51-2R REPAIR 10. THIS IS MAJOR REPAIR.
- [SDR FDEA202506261062](https://openairdocs.org/sdr/FDEA202506261062.md): Battery Pack · inoperative · Jun 26, 2025 · N901FD · Boeing 7572B7 · Emergency Lighting
  > CENTER AND RIGHT EMERGENCY EXIT SIGNS IN GALLEY FAIL TO LIGHT WHEN TESTED FOR SERVICE CHECK. AMM: 33-51-07-2 REMOVED AND REPLACED FOWARD GALLEY EMERGENCY LIGHTING BATTERY PACK REF 757MM 33-51-07-2.CENTER AND RIGHT EMERGENCY EXIT LIGHT OPS CHECK GOOD PER

Next page: https://openairdocs.org/model/boeing-757-2b7/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 aircraft_model_key = '7572B7'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-2b7/reports

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