# Service difficulty reports: Boeing 757-2T7

A list on [Boeing 757-2T7](https://openairdocs.org/model/boeing-757-2t7.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 14 · 666 reports

- [SDR FDEA202610131587](https://openairdocs.org/sdr/FDEA202610131587.md): Indication Sys · malfunctioned · Oct 13, 2026 · N935FD · Boeing 7572T7 · Hydraulic Indicating System
  > DURING CLIMB OUT, GOT RT HYD SYS PRESSURE EICAS & ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE & NORMAL QUANTITY. EMERGENCY DECLARED. IAW CHAPTER 6, AMM 26-18-00-5, AMM 29-11-00-5, AMM 28-22-00-5, AMM 75-32-01-2, AMM 73-2
- [SDR FDEA202610131564](https://openairdocs.org/sdr/FDEA202610131564.md): Wire · shorted · Oct 13, 2026 · N935FD · Boeing 7572T7 · Hydraulic Indicating System
  > DURING CLIMB OUT GOT R HYD SYS PRESS EICAS AND ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE AND NORMAL QUANTITY. EMERGENCY DECLARED. FOUND WIRE W5200-0073-20 SHORTED TO GROUND. REMOVED CONTACTS 2 & 3 OF C/P D3064 & SHORT T
- [SDR FDEA202609181374](https://openairdocs.org/sdr/FDEA202609181374.md): Eec · failed · Sep 18, 2026 · N935FD · Boeing 7572T7 · Fuel Controlling System
  > L EEC EICAS DURING TAKEOFF ROLL AND 4X IN FLIGHT ALL WITH ASSOCIATED AUTOTHROTTLES EICAS. NOTABLE YAW IN FLIGHT WHEN IT WOULD OCCUR. COMPLIED WITH QRH. FIM: 73-21 FAULT TREE 822 ON HIGH POWER RUN FOUND LH EEC WENT TO OFF AS THROTTLES WERE INCREASED. PER
- [SDR FDEA202609141333](https://openairdocs.org/sdr/FDEA202609141333.md): Gust Lock · failed · Sep 14, 2026 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > WHILE CLOSING THE L-1 DOOR, RAMP WAS UNABLE TO RELEASE THE GUST LOCK. FOUND HOLD OPEN DOOR COLLAR DAMAGED AND WILL REQUIRE REPLACEMENT. PART NIS AT FLL. AMM 52-11-08-8 REMOVED AND REPLACED L1 DOOR HOLD OPEN SPLIT COLLAR ASSY IAW AMM 52-11-08-8. L1 DOOR
- [SDR FDEA202607231013](https://openairdocs.org/sdr/FDEA202607231013.md): Beam · corroded · Jul 23, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Structure
  > NOSE WHEEL WELL STRUCTURE BS 310.5 LOWER AREA INTERNAL BEAM WITH CORROSION REMOVED VERTICAL BEAM OUT OF LIMITS AT NOSE WEEL STRUCTURE BS 310.5 LBL 20.05 LOWER AREA INTERNAL IAW B757 51-40-02-0G; TRIMED LOCATED, DRILLED AND INSTALLED NEW VERTICAL BEAM REPLA
- [SDR FDEA202607200955](https://openairdocs.org/sdr/FDEA202607200955.md): Strap · corroded · Jul 20, 2026 · N935FD · Boeing 7572T7 · Fuselage Miscellaneous Structure
  > APU INLET DUCT ATTACHMENTS AT THE AFT FRAME WITH CORROSION CORRSION OUT OF LIMITS AT APU INLET DUCT ATTACHMENTS ON THE AFT FRAME (MIDDLE STRAP) IAW B-757 SRM 53-80-15-1A WAS REPAIRED IAW B-757 SRM 53-80-15-2R REPAIR 1
- [SDR FDEA202607200954](https://openairdocs.org/sdr/FDEA202607200954.md): Crease Beam · corroded · Jul 20, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Structure
  > MCC CREASE BEAM SIDE LH BSTA 1620 TO BSTA 1370 IT HAS CORROSION SPOTS MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1430 TO 1530 LBL 64.40 IAW B-757 SRM 53-60-13-1A, WAS REPAIRED IAW B-757 SRM 53-00-13-2R REPAIR 1
- [SDR FDEA202607200953](https://openairdocs.org/sdr/FDEA202607200953.md): Crease Beam · corroded · Jul 20, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Structure
  > MCC SIDE LH BETWEEN BS 1080 TO BS 1100 CREASE BEAM WITH CORROSION MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1040 TO STA 1100 IAW B-757 SRM 53-40-13-1A WAS REPAIRED IAW B-757 SRM 53-40-13-1A, WAS REPAIRED IAW B-757 SRM 53-00-13-2R R
- [SDR FDEA202607150928](https://openairdocs.org/sdr/FDEA202607150928.md): Floorbeam · corroded · Jul 15, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Floor Beam
  > MCC BL 0 TO LBL 24.75 BS 1200 FLOOR BEAM WITH CORROSION AREA WITH CORROSION OUT OF LIMITS AT FLOOR BEAM BS 1200 LBL 8 TO LBL 14 WAS REPAIRED IAW B757 SRM 53-00-51-2R REPAIR 5
- [SDR FDEA202607150927](https://openairdocs.org/sdr/FDEA202607150927.md): Collar · broken · Jul 15, 2026 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK FOUND BROKEN DURING POST FLIGHT CHECK UPON FLIGHT ARRIVAL. REINSTALLED NEW AND SERVICEABLE GUST LOCK AS REQUIRED, OPS CHECK GOOD IAW AMM 52-11-08-8.
- [SDR FDEA202607100893](https://openairdocs.org/sdr/FDEA202607100893.md): Skin Panel · dented · Jul 10, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I.A.W B757 SRM 53-80-01-1A, TABLE I, NOTE 'C', FIG 101, SHEET 2 AND SRM 51-70-10-2R REP '4'
- [SDR FDEA202607100892](https://openairdocs.org/sdr/FDEA202607100892.md): Access Panel · cracked · Jul 10, 2026 · N935FD · Boeing 7572T7 · Wing, Plate/Skin
  > LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523GB AREA WITH 02 EA CRACK. 2EA CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523GB AREA WERE REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4
- [SDR FDEA202607100890](https://openairdocs.org/sdr/FDEA202607100890.md): Access Panel · cracked · Jul 10, 2026 · N935FD · Boeing 7572T7 · Wing, Plate/Skin
  > LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523FB AREA WITH 01EA CRACK. CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523FB AREA WAS REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4.
- [SDR FDEA202605280640](https://openairdocs.org/sdr/FDEA202605280640.md): Gust Lock · damaged · May 28, 2026 · N937FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK IS BROKEN. TROUBLESHOOTING REQUIRED PRIOR TO INSTALLING IPC EFFECTIVITY VERIFICATION IS ALSO REQUIRED. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR AND OPS CHKD GOOD IAW AMM 52-11-08-4.
- [SDR FDEA202601060008](https://openairdocs.org/sdr/FDEA202601060008.md): Skin · corroded · Jan 6, 2026 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > ENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA IS WITH CORROSION AREA WITH CORROSION AT ENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA WAS REPAIRED PER FEDEX E.A. #: F-5430-T0385801 P1 WITH TITLE: NACELLES / PYLONS - - SKIN /
- [SDR FDEA202601060007](https://openairdocs.org/sdr/FDEA202601060007.md): Crease Beam · cracked · Jan 6, 2026 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > RH LOBE INTERIOR BETWEEN BS 1720 AND STR 17 HAS CREASE BEAM WITH CRACK 2 INCH APROX. ACCOMPLISHED REPAIR ON ADDITIONAL DAMAGE FOUND: CRACK IN THE HOLE AT AFT PRESSURE BULKHEAD STA 1720 PER FEDEX E.A.#: F-5310-T0385818 P1 WITH TITLE: FUSELAGE - MAINFRAME -
- [SDR FDEA202512302297](https://openairdocs.org/sdr/FDEA202512302297.md): Skin · corroded · Dec 30, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NACELLE STRUT PP STA 174.30 R/H FWD BULKHEAD INTERNAL SIDE SKIN WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A.#: F - 5430 - T0385806 P1 WITH TITLE: NACELLES/PYLONS - SKIN/PLATES/PANELS - RN 1 PYLON INBD SIDE SKIN INNER SURFACE CORROS
- [SDR FDEA202512302296](https://openairdocs.org/sdr/FDEA202512302296.md): Skin · corroded · Dec 30, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NACELLE STRUT ACCESS PANEL 433JR CUTOUT WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A F- 5430 - T0385806 P1
- [SDR FDEA202512292295](https://openairdocs.org/sdr/FDEA202512292295.md): Stringer · corroded · Dec 29, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Longeron/Stringer
  > MEC BETWEEN BS 418 - 440, S24R CORRODED. PERMANENTLY REPAIRED STRINGER 24R IAW SRM 53-00-03-2R, REP 2, FIG 201.
- [SDR FDEA202512272292](https://openairdocs.org/sdr/FDEA202512272292.md): Skin · corroded · Dec 27, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NO 1 ENGINE NACELLE BETWEEN ACCESS PANEL 433 HR AND 433 JR INTERNAL SKIN WITH CORROSION. JOBS FOR NR W/O 91519, N00437 AND N00438 WAS INCLUDED AND ACCOMPLISHED UNDER FEDEX EA F-5430-T0385806 P1
- [SDR FDEA202512222284](https://openairdocs.org/sdr/FDEA202512222284.md): Crease Beam · corroded · Dec 22, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MAIN CABIN. CREASE BEAM. (RH) STA 1200 CORRODED. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT CREASE BEAM INBOARD CHORD AT STA 1200 RBL 64 WAS REPAIRED IAW B-757 SRM 53-00-13-2R
- [SDR FDEA202512222283](https://openairdocs.org/sdr/FDEA202512222283.md): Crease Beam · corroded · Dec 22, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MCC FLOOR BTWN STA 440 - 460 (RH CREASE BEAM) RBL 64.5 APROX WAS FOUND ON LOCATION WITH CORROSION. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT, CREASE BEAM INBOARD CHORD BTW STA 440-460 RBL 64.40 WAS REPAIRED IAW B-757 SRM 53-00-13-2R
- [SDR FDEA202512222282](https://openairdocs.org/sdr/FDEA202512222282.md): Crease Beam · corroded · Dec 22, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MAIN CARGO BAY, FLOOR INBOARD CHORD HAS SURFACE CORROSION AROUND NUTS PLATE BETWEEN BS 860 AND 879 CORROSION OUT OF LIMITS AT MAIN CARGO BAY CREASE BEAM INBOARD CHORD BTW STA 860 - 879 RBL 64 WAS REPAIRED IAW SRM 53-00-13-2R.
- [SDR FDEA202512192264](https://openairdocs.org/sdr/FDEA202512192264.md): Skin · corroded · Dec 19, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > ENG NR 2 NACELLE STRUT FWD ACCESS PANEL 443AR INSIDE SKIN IS WITH CORROSION. (INNER AREA.) ENG. NR 2 NACELLE STRUT OTBD SIDE FWD ACCESS PANEL 443AR SKIN OUT OF LIMITS WAS REPLACED IAW SRM 51-41-02-0G AND DWG 311N5041 REV. K.
- [SDR FDEA202512172260](https://openairdocs.org/sdr/FDEA202512172260.md): Deck Plate · corroded · Dec 17, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > POINTS NR 2 AND 3 WITH CORROSION OUT OF LIMITS AT DECK PLATE AREA, BS 1681, BTW RBL 13 - 23, OUT OF LIMITS AT CABIN DECK PLATE. REPAIRED IAW SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE II.
- [SDR FDEA202512172259](https://openairdocs.org/sdr/FDEA202512172259.md): Skin · corroded · Dec 17, 2025 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/Skin
  > NR 2 NACELLE STRUT FWD ACCESS PANEL 443GL INSIDE SKIN AREA IS WITH CORROSION. NR 2 NACELLE STRUT INBD SIDE FWD ACCESS PANEL 443GL SKIN OUT OF LIMITS WAS REPLACED IAW SRM 51-41-02-0G AND DWG 311N5041, REV. K
- [SDR FDEA202512122247](https://openairdocs.org/sdr/FDEA202512122247.md): Shear Web · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SHEAR WEB HAD MULTIPLES SPOTS OF CORROSION, BS 1680 - 1720, AREA OUT OF LIMITS. BS 1697, LBL 08 IAW SRM 53-60-51-1A. REPAIRED IAW SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE II.
- [SDR FDEA202512122246](https://openairdocs.org/sdr/FDEA202512122246.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BAY SEAT TRACK 45.50 RBL BETWEEN BS 1100 -1140 HAS MULTIPLE AREAS WITH CORROSION. REMOVED SEAT TRACK BS 1076 TO 1180, RBL 45.50 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 51-40-05-0G, SRM 51
- [SDR FDEA202512122245](https://openairdocs.org/sdr/FDEA202512122245.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BAY, SEAT TRACK 45.50 LBL BETWEEN BS 1180 - 1200 WITH CORROSION IN MULTIPLES AREAS. REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 1180 TO 1240, LBL 45.50 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED NEW SEAT TRACK REPLAC
- [SDR FDEA202512122244](https://openairdocs.org/sdr/FDEA202512122244.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BAY FLOOR SEAT TRACK HAS SURFACE CORROSION BETWEEN BS 680 & 720, RBL 58.22. REMOVED SEAT TRACK SECTION OUT LIMITS AT MAIN CARGO BS BS 640 - 880, RBL 58.22 IAW SRM 51-40-02-0G. TRIMED, LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-05
- [SDR FDEA202512122243](https://openairdocs.org/sdr/FDEA202512122243.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN. SEAT TRACK, RBL 58.22 BTW BS 1180 TO 1200 CORRODED REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT BS 1180 TO 1420 RBL 58.22 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED A NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 5
- [SDR FDEA202512122242](https://openairdocs.org/sdr/FDEA202512122242.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BAY SEAT TRACK LBL 58.22, BS 1180 - 1420 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION IAW SRM 51-40-02-0G. TRIMMED, LOCATED, DRILLED AND INSTALLED A NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 51-40-05-0G, SRM 51-40-08-0G, SRM
- [SDR FDEA202512122241](https://openairdocs.org/sdr/FDEA202512122241.md): Seat Track · corroded · Dec 12, 2025 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARMENT SEAT TRACK LBL BETWEEN BS 1180 - 900 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 900 - 1180, LBL 58.22 IAW SRM 51-40-02-0G; TRIMMED, LOCATED, DRILLED AND INSTALLED A NEW SEAT TRAC
- [SDR FDEA202512122240](https://openairdocs.org/sdr/FDEA202512122240.md): Skin · delaminated · Dec 12, 2025 · N937FD · Boeing 7572T7 · Trailing Edge Flaps
  > LEFT WING OTBD MAIN FLAP T/E UPPER SURFACE HAD POSSIBLE DELAMINATION. APPLIED PERMANENT REPAIR ON AREAS WITH DELAMINATION AT LT WING OTBD MAIN FLAP T/E UPPER SURFACE BTW WBL 471 - WBL 501 IAW SRM 57-53-01-2R, TABLE III, AND SRM 51-70-07-0G.
- [SDR FDEA202512112237](https://openairdocs.org/sdr/FDEA202512112237.md): Crease Beam · corroded · Dec 11, 2025 · N937FD · Boeing 7572T7 · Fuselage Main, Structure
  > MAIN CARGO BAY FLOOR CREASE BEAM HAS SURFACE CORROSION BETWEEN BS 760 AND 780. REMOVED CREASE BEAM INBD CHORD SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT LBL 64.20 BS 760 TO 900 IAW B757 SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED AND INSTALLED NEW CREASE
- [SDR FDEA202512102230](https://openairdocs.org/sdr/FDEA202512102230.md): Skin · dented · Dec 10, 2025 · N937FD · Boeing 7572T7 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB UPPER SKIN HAD REPAIR DAMAGE AT LOWER INTERNAL SURFACE, HSS 104.248 & 128.248, DENT WITH DELAMINATION AT LT HORIZONTAL STAB UPPER SKIN ON LOWER INTERNAL SURFACE WAS APPLIED PERMANENT REPAIR IAW SRM 55-10-01-1A, TABLE 1, NOTE I, & SRM 51-
- [SDR FDEA202512102229](https://openairdocs.org/sdr/FDEA202512102229.md): Skin · dented · Dec 10, 2025 · N937FD · Boeing 7572T7 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB UPPER SKIN HAD FIVE DENTS BETWEEN HSS 81.249 AND 104.248, APPLIED PERMANENT REPAIR AT LT HORIZONTAL STAB UPPER SKIN IAW SRM 55-10-01-1A, TABLE I NOTE I & SRM 51-70-10-2R
- [SDR FDEA202506060850](https://openairdocs.org/sdr/FDEA202506060850.md): Gust Lock · inoperative · Jun 6, 2025 · N935FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK FOUND DAMAGED/BROKEN ON WALKAROUND. AMM: 52-11-08-8 INSTALLED NEW SPLIT COLLAR IRW AMM 52-11-08-8.
- [SDR FDEA202408301193](https://openairdocs.org/sdr/FDEA202408301193.md): Transmission · dirty · Aug 30, 2024 · N937FD · Boeing 7572T7 · Trailing Edge Flap Actuator
  > TE FLAP DISAGREE ON APPROACH. FLAPS STUCK BETWEEN 20-25 DEGREES. EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING PER FIM. FOUND FAULT CODE 305 (FLAP DISAGREE) ON FSEU-1. PERFORMED VISUAL INSPECTION OF ALL FLAP DRIVE TRANSMISSIONS AND JACKSCREWS. FOUND FLAP #5
- [SDR FDEA202408171144](https://openairdocs.org/sdr/FDEA202408171144.md): Stringer · corroded · Aug 17, 2024 · N935FD · Boeing 7572T7 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO LSTR 19-22 STA 760 FRAME HAS AREAS OF CORROSION AT SKIN ATTACHMENT POINTS AND STR EVALUATED CORROSION AT SKIN ATTACHMENT POINTS S-19L, 21L, AND 22L NO CORROSION NOTED. REPAIRED STRINGER WITH SPLICE, SHEAR TIE, AND FILLER BETWEEN S-19L TO 20L
- [SDR FDEA202406280877](https://openairdocs.org/sdr/FDEA202406280877.md): Battery · no test · Jun 28, 2024 · N937FD · Boeing 7572T7 · Emergency Lighting
  > LEFT SIDE EMERGENCY LIGHTS DO NOT TEST. R & R LT EMERGENCY LIGHTS POWER SUPPLY REF 757 AMM 33-51-07-2. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR FDEA202406120794](https://openairdocs.org/sdr/FDEA202406120794.md): Battery · no test · Jun 12, 2024 · N937FD · Boeing 7572T7 · Emergency Lighting
  > DURING EMERGENCY EXIT LIGHT TEST R/H EXIT LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. R/H EXIT LIGHT OPS CHK SERVICEABLE. OK TO CONTINUE.
- [SDR FDEA202403300423](https://openairdocs.org/sdr/FDEA202403300423.md): Battery Pack · inoperative · Mar 30, 2024 · N935FD · Boeing 7572T7 · Emergency Lighting
  > THROUGHOUT MAINTANENCE DAILY CHECK FOUND L1 EMER EXIT SIGN DOOR 1 LT, FLT DECK DOME EMER LT MODULE, SLIDE LT DR 1 EMER INOP. SHGN 30MAR24 05:49 BNA WDM: CH 33-51-12 PG 13.1 SHEET 1FX1 PERFORMED T/S PROCEDURES TO EMERGENCY LIGHTS FORWAR LEFT SIDE L1 D
- [SDR FDEA202403160300](https://openairdocs.org/sdr/FDEA202403160300.md): Girt Bar · out of alignment · Mar 16, 2024 · N935FD · Boeing 7572T7 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE BEGAN TO FALL OUT WHEN DOOR WAS OPENED FOR CREW STAIR MATING. DURING TROUBLESHOOTING FOUND LH DOOR AFT FLOOR FITTING MISALIGNED. RE-ALIGNED FITTING IAW AMM 25-66-10-2. REINSTALLED GIRT BAR ON LT DOOR AND OPS CHECKED PER THE ABOVE MANUAL
- [SDR FDEA202402210206](https://openairdocs.org/sdr/FDEA202402210206.md): Fitting · damaged · Feb 21, 2024 · N937FD · Boeing 7572T7 · Wing Main, Frame Structure
  > DURING ACCOMPLISHED W/C EF-5730-E0340076 P11 STEP #3 PAGE 5 OF 13. FOUND #8 HOLE 2ND OVERSIZED. REMOVED & REINSTALLED #1 ENG IB & OB FAN COWLS, #1 PYLON BULLNOSE, IB TORQUE TUBE BTWN SLAT 4 & 5, Y-DUCT, LUBE FITTING, FUEL SUPPLY LINE & UPPER LINK IAW B757
- [SDR FDEA202401240105](https://openairdocs.org/sdr/FDEA202401240105.md): Skin · dented · Jan 24, 2024 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > DENT FOUND AT FUSELAGE SKIN BTW STA 480-500, STR 22-R TO 23R. EVALUATED DENT ON FUSELAGE SKIN BETWEEN STA 480-500, STR 22R TO 23R FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-01-1A, FIG 101 DETIAL III, CUT DAMAGED AREA IAW B757 SRM 53-00- 01-2R PAR 4 D, PER
- [SDR FDEA202401230102](https://openairdocs.org/sdr/FDEA202401230102.md): Skin · gouged · Jan 23, 2024 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 497 1 1/8" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND IN LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINATIN
- [SDR FDEA202401230101](https://openairdocs.org/sdr/FDEA202401230101.md): Skin · gouged · Jan 23, 2024 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 490 0.787" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND OUT OF LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMIN
- [SDR FDEA202401190091](https://openairdocs.org/sdr/FDEA202401190091.md): Floor Panel · dented · Jan 19, 2024 · N937FD · Boeing 7572T7 · Fuselage Floor Panel
  > MAIN CABIN FOUND DENTS ON FLOORBOARD PANEL #232 MJF BETWEEN STA 560 TO STA 680 RBL 58.22 TO RBL 63.5.
- [SDR FDEA202208071908](https://openairdocs.org/sdr/FDEA202208071908.md): Frame · delaminated · Aug 7, 2022 · N935FD · Boeing 7572T7 · Elevator Structure
  > LEFT ELEVATOR O/B UPPER SURFACE CONDUCTIVE FRAME IS DELAMINATED. REMOVED & REPLACED -7 ADAPTER PLATE IAW DWG 183N2003 REV G, -5 SPLICE PLATE & CONDUCTIVE FRAME IAW SRM 51-40-02 & DWG 183N2003 REV G & AMM 55-29-00-8.

Next page: https://openairdocs.org/model/boeing-757-2t7/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 = '7572T7'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-2t7/reports

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