# Service difficulty reports: N940FD

A list on [N940FD](https://openairdocs.org/aircraft/N940FD.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 3 · 126 reports

- [SDR FDEA202308081372](https://openairdocs.org/sdr/FDEA202308081372.md): Unknown · unknown · Aug 8, 2023 · N940FD · Boeing 757200 · Pitot/Static Anti-Ice System
  > AFTER TO, TAT EICAS MESSAGE. RAN QRH, AND RETURNED TO RST. ***EMERGENCY DECLARED*** RELEASED FOR SERVICE PER MEL: 30-33-01-01
- [SDR FDEA202301090052](https://openairdocs.org/sdr/FDEA202301090052.md): Power Supply · failed · Jan 9, 2023 · N940FD · Boeing 757236 · Emergency Lighting
  > DURING SERVICE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED L1 DOOR EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51-07-2 STEPS 6. AND 7. OPS TEST GOOD.
- [SDR FDEA202202150302](https://openairdocs.org/sdr/FDEA202202150302.md): Frame · cracked · Feb 15, 2022 · N940FD · Boeing 757200 · Standard Practices/Structures
  > BS 1640 S-14R I/B BOTTOM HOLE HAS CRACK INDICATIONS AT 4 & 9 O'CLOCK LOOKING AFT // BS 1640 S-14R O/B BOTTOM HOLE HAS A CRACK INDICATION AT 5 O'CLOCK LOOKING AFT. ACCOMPLISHED FRAME REPAIR AT STA. 1640 BTW STR. 9 & STR 20 IAW EA # F-5310- T0366462 "FUSELAG
- [SDR FDEA202202070249](https://openairdocs.org/sdr/FDEA202202070249.md): Frame · cracked · Feb 7, 2022 · N940FD · Boeing 757200 · Standard Practices/Structures
  > BS 1640 S-14L I/B BOTTOM HOLE HAS A CRACK INDICATION AT 8 O'CLOCK LOOKING AFT. COMPLIED WITH ALL STEPS TO COMPLETION 1-10 OF EA T F-5310-T0366488 P1 FUSELAGE - MAINFRAME - CRACK INDICATION AT STA 1640 FUSELAGE FRAME WEB, S-14L AT LOWER INBOARD HOLE LO
- [SDR FDEA202106141535](https://openairdocs.org/sdr/FDEA202106141535.md): Clamp · unsecure · Jun 14, 2021 · N940FD · Boeing 757236 · Engine (Turbine/Turboprop)
  > ON CLIMB OUT PASSING 16000 EICAS MESSAGE L ENG OVHT. LEVELED AT 19000 TO COMPLY WITH QRH 8.1.20. L ENG THROTTLE WAS BROUGHT TO IDLE AND MESSAGE CLEARED AFTER APPROXIMATELY 30 SECONDS. CONTINUED CLIMB TO 350 AND CONTINUED TO DESTINATION WITH NO FURTHER ISS
- [SDR FDEA202105011079](https://openairdocs.org/sdr/FDEA202105011079.md): Girt Bar · detached · May 1, 2021 · N940FD · Boeing 757236 · Emergency Equipment
  > UPON OPENING R1 DOOR, NOTICED GIRT BAR SLIDER HAD FALLEN OFF. WHILE ATTEMPING TO SECURE SLIDER, R1 DOOR SLIDE LIBERATED FROM DOOR. ACCOMPLISHED ADJUSTMENT/TEST OF R1 DOOR GIRT BAR PER B757-200 AMM 52-11-25-5, FOUND LEAF SPRING ON FWD END OF GIRT BAR BENT A
- [SDR FDEA202103300799](https://openairdocs.org/sdr/FDEA202103300799.md): Fire Warning · false activation · Mar 30, 2021 · N940FD · Boeing 757236 · Fire Detection
  > PDIS 940 26-10 7568 30MAR21 JAX FACT U AT CRUISE GOT INTERMITTENT L ENGINE FIRE WARNINGS. ALL ENGINE INDICATIONS AND AIRCRAFT PERFORMANCE NORMAL. AFTER APPROXIMATELY 3 MINUTES OF INTERMITTENT WARNINGS THEY STOPPED AND DID NOT OCCUR AGAIN DURIN
- [SDR FDEA202103270787](https://openairdocs.org/sdr/FDEA202103270787.md): Slide · low pressure · Mar 27, 2021 · N940FD · Boeing 757236 · Escape Slide
  > L1 DOOR EMERGENCY SLIDE PRESSURE INDICATING IN RED. REMOVED AND REPLACED L1 DOOR SLIDE/RAFT PER AMM 25-66-01-4.
- [SDR FDEA2020072311600](https://openairdocs.org/sdr/FDEA2020072311600.md): Sensor · unsecure · Jul 21, 2020 · N940FD · Boeing 757236 · Windshield/Door Rain/Ice Removal
  > REJECTED T/O AT 50 KNOTS. ECIAS DISPLAYED RT SIDE WINDOW PERFORMED REJECTED T/O CHECK LIST IN QRH. FOUND THE R3 WINDOW SENSOR MOUNT LOOSE. SECURED THE SENSOR MOUNT. PERFORMED WINDOW HEAT ADJUSTMENT AND TEST IAW MM 30-41-01-03 AND CHECKED NORMAL. ACFT OK F
- [SDR FDEA202002070281](https://openairdocs.org/sdr/FDEA202002070281.md): Skin · dented · Feb 7, 2020 · N940FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STAB UPPER SKIN AUX SPAR PREVIUS REPAIR APROX.. 4" 3/4 CIRCUNFERENCE DELAM AT STA 78.00 REMOVED EXISTING REPAIR AND ACCOMPLISHED PERMENENT REPAIR ON R/H HORIZONTAL STAB UPPER SKIN AT STA 78 IAW B757 SRM 55-10-01-1A AND IAW B757 SRM 51-70
- [SDR FDEA20200130236](https://openairdocs.org/sdr/FDEA20200130236.md): Beam · gouged · Jan 29, 2020 · N940FD · Boeing 757236 · Cargo/Baggage Doors
  > 3EA SMALL GOUGES - MAIN CARGO DOOR VERTICAL BEAM INBD CHORD INTERIOR SURFACE - APPROX STA 490,BETWEEN WATER LINE 210 - 215. REMOVED GOUGES ON MAIN CARGO DOOR VERTICAL BEAM I\B CHORD APPROX STA 490 BETWEEN WL 210-215 IAW B757 SRM 51-40-02. FOUND TO BE OUT
- [SDR FDEA2020013090238](https://openairdocs.org/sdr/FDEA2020013090238.md): Shear Tie · corroded · Jan 29, 2020 · N940FD · Boeing 757236 · Fuselage Internal Mounting Structure
  > AFT LOWER CARGO COMPARTMENT, CORROSION, SHEAR TIE STA 1480 BETWEEN STR 28R AND STR 29R. REMOVED CORROSION ON SHEAR TIE AT STA 1480 BETWEEN STR 28R-29R IAW SRM 51-10-02-0G. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DET 2. REMOVED SHEAR TIE IAW SRM 5
- [SDR FDEA2020012320198](https://openairdocs.org/sdr/FDEA2020012320198.md): Floorbeam · corroded · Jan 22, 2020 · N940FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN DECK STA 1055 BETWEEN BL0-RBL 24.75 FLOOR SUPPORT CORRODED. ACCOMPLISHED IAW EA F-5310-T0352036 P1 FUSELAGE - MAINFRAME -MAIN CARGO FLOOR SUPPORT STA 1055 CORRODED, NEW PART FABRICATION TEMPER ATERATION, REMOVED CORR IAW SRM 51-10-02-OG, FOUND TO BE OUT L
- [SDR FDEA202001210190](https://openairdocs.org/sdr/FDEA202001210190.md): Seat Track · corroded · Jan 21, 2020 · N940FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK FLANGE CORRODED BETWEEN STA 1180 - 1200 RBL 45.5. REMOVED CORROSION ON SEAT TRACK FLANGE AT STA 1180 TO 1200, RBL 45.5 IAW SRM 51-10-02-OG. EVALUATED DAMAGED AREA, ORIG MAT =.070', REM MAT =.040",MAT LOSS =.030" FOUND TO BE OUT LIMITS IA
- [SDR FDEA2020012170162](https://openairdocs.org/sdr/FDEA2020012170162.md): Fitting · cracked · Jan 17, 2020 · N940FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT SHEAR WEB STRUCTURE CLIP IS CRACKED AT O/B RBL 24.75" AND BS 1715. REMOVED, FABRICATED AND INSTALLED CLIP ON AFT CARGO COMP SHEAR WEB STRUCTURE AT O/B SIDE OF RBL 24.75, STA 1715 IAW SRM 51-40-02-OG AND B DWG 146N5329,REV - AND REV C.
- [SDR FDEA202001170159](https://openairdocs.org/sdr/FDEA202001170159.md): Shear Tie · cracked · Jan 17, 2020 · N940FD · Boeing 757236 · Emergency Exits
  > FUSELAGE LT EMERGENCY EXIT INTERNAL STRUCTURE AT MID SECTION AFT STIFFENER CRACKED BETWEEN STR 13L TO STR 14L ON STA 1340. (SHEAR TIE) REMOVED AND REPLACED STIFFENER (SHEAR TIE) ON LT EMERGENCY EXIT DOOR AT INTERNAL STRUCTURE MID SECTION AFT SIDE IAW SRM 51-40
- [SDR FDEA202001110112](https://openairdocs.org/sdr/FDEA202001110112.md): Skin · cracked · Jan 11, 2020 · N940FD · Boeing 757236 · Service Doors
  > MAIN CABIN R2 DOOR ENTRY DOOR UPPER HINGE CUT OUT CRACKED. COMPLIED WITH EA #: F-5210-T0351839 P1 TITLE: DOORS - PASSENGER / CREW - R-2 DOOR FOWARD FRAME UPPER HINGE CUT OUT SRM REPAIR - RSC TRACKING AND B 757 SRM 52-10-02-2R FIG 201 REP 1 DET III.
- [SDR FDEA2020011310112](https://openairdocs.org/sdr/FDEA2020011310112.md): Hinge · cracked · Jan 11, 2020 · N940FD · Boeing 757236 · Fuselage, Door Hinge
  > MAIN CABIN R2 DOOR ENTRY DOOR UPPER HINGE CUT OUT CRACKED. COMPLIED WITH FEDEX EA #: F-5210-T0351839 P1 TITLE: DOORS - PASSENGER / CREW - R-2 DOOR FOWARD FRAME UPPER HINGE CUT OUT SRM REPAIR - RSC TRACKING AND B 757 SRM 52-10-02-2R FIG 201 REP 1 DET III.
- [SDR FDEA201805181256](https://openairdocs.org/sdr/FDEA201805181256.md): Line · failed · May 18, 2018 · N940FD · Boeing 757236 · Hydraulic System, Main
  > GEAR DOORS EICAS MESSAGE DURING FINAL. REMOVED AND REPLACED THE FWD RETRACT HYD LINE ON THE RT MAIN LANDING GEAR DOOR ACTUATOR IAW AMM 20-10-10-4. PERFORMED AN OPS CHECK OF THE MAIN LANDING GEAR DOOR IAW AMM 32-32-12-4, PARA 3.G. OPS AND LEAK CHECKED GOOD.
- [SDR FDEA201801140091](https://openairdocs.org/sdr/FDEA201801140091.md): Girt Bar · bent · Jan 14, 2018 · N940FD · Boeing 757236 · Emergency Equipment
  > LEFT L1 DOOR GIRT BAR TAB BENT. REMOVED AND REPLACED L1 DOOR GIRT BAR IN REF TO AMM 25-6601-4. OPS CHECK NORMAL. OK TO CONTINUE.
- [SDR FDEA201705011302](https://openairdocs.org/sdr/FDEA201705011302.md): Battery Pack · no test · May 1, 2017 · N940FD · Boeing 757236 · Emergency Lighting
  > RH EMERGENCY EXIT LIGHTS NOT TESTING. REMOVED AND REPLACED THE M730 POWER SUPPLY BATTERY PACK IAW AMM 33-51-07-2, OPS CHECKED GOOD
- [SDR FDEA201610253684](https://openairdocs.org/sdr/FDEA201610253684.md): Sign · malfunctioned · Oct 25, 2016 · N940FD · Boeing 757236 · Emergency Lighting
  > CENTER CEILING EXIT SIGN AND R1 DOOR EXIT SIGN DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. EMERGENCY LIGHTS OP CHECKS GOOD IAW MM 33-51-00-5. OK FOR SERVICE.
- [SDR FDEA201610253683](https://openairdocs.org/sdr/FDEA201610253683.md): Light · malfunctioned · Oct 25, 2016 · N940FD · Boeing 757236 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT BEHIND R1 DOOR NOT ILLUMINATED DURING EMERGENCY LIGHT TEST. EMERGENCY LIGHTS OP CHECKS GOOD. IAW MM 33-51-00-5. OK FOR SERVICE.
- [SDR FDEA201510293404](https://openairdocs.org/sdr/FDEA201510293404.md): Girt Bar · obstructed · Oct 29, 2015 · N940FD · Boeing 757236 · Emergency Equipment
  > RIGHT ENTRY DOOR DIFFICULT TO ARM. INSPECTED GIRT BAR ASSEMBLY IAW AMM 25-66-01-6. FOUND FOD IN DOOR SILL AREA NOT ALLOWING GIRT BAR TO REACH FLOOR LEVEL WHEN ARMED. REMOVED FOD & SLIDE NOW ARMS & DISARMS WITHOUT EFFORT. ACFT OK FOR SERVICE AT THIS TIME.
- [SDR FDEA201509292998](https://openairdocs.org/sdr/FDEA201509292998.md): Retainer · out of position · Sep 29, 2015 · N940FD · Boeing 757236 · Wheel/Ski/Float
  > WHEN RAISING GEAR ON TAKEOFF, HAD BIG VIBRATION FROM MAIN GEAR. AMBER DOOR & GEAR LIGHTS STAYED ILLUMINATED LONGER THAN USUAL, VERY NOISY. UPON INSPECTION FOUND RT NOSE WHEEL ASSEMBLY INBD BEARING RETAINER RING POPPED OUT & HANGING ON AXLE HOUSING. REPLACED
- [SDR FDEA201505101457](https://openairdocs.org/sdr/FDEA201505101457.md): Reservoir · inoperative · May 10, 2015 · N940FD · Boeing 757236 · Passenger/Crew Doors
  > ON BLOCK IN, FOUND R1 DOOR 1/2 OPEN WITH GRIT BAR STILL CONNECTED TO DOOR LOWER FRAME. REPLACED R1 DOOR EMER POWER RESERVOIR IAW MM 52-11-30-4. OPERATIONS NORMAL..
- [SDR FDEA201411263897](https://openairdocs.org/sdr/FDEA201411263897.md): Light · inoperative · Nov 26, 2014 · N940FD · Boeing 757236 · Door Warning System
  > LEFT MAIN CABIN DOOR WOULD NOT SHOW ARM SLIDE CORRECTLY. RELAMPED SLIDE ARMED WARNING LIGHT IAW SMP. LIGHT NOW FUNCTIONS WHEN DOOR IS ARMED.
- [SDR FDEA201403280595](https://openairdocs.org/sdr/FDEA201403280595.md): Actuator · failed · Mar 28, 2014 · N940FD · Boeing 757236 · Leading Edge Slat Actuator
  > DURING DEPARTURE, WHEN FLAPS SELECTED TO UP THE LE SLAT DISAGREE EICAS CAME ON. THE LE DISCREET LIGHT ILLUMINATED. R & R NR 6 OTBD LE SLAT DRIVE ROTARY ACTUATOR IAW MM 27-81-18-4. OPS CHECKED GOOD.
- [SDR FDEA201401260201](https://openairdocs.org/sdr/FDEA201401260201.md): Shear Tie · cracked · Jan 26, 2014 · N940FD · Boeing 757236 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CRACKED AT BS 1300 BETWEEN STRINGER 20 - 21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW & INSTALLED IAW DWG 146N2002 REV EU & SRM 51-40-02.
- [SDR FDEA201312183001](https://openairdocs.org/sdr/FDEA201312183001.md): Fseu · inoperative · Dec 18, 2013 · N940FD · Boeing 757236 · Leading Edge Slat Control System
  > LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED DURING CONFIGURATION. FOLLOWED QRH, UNEVENTFUL LANDING. T/S PER FIM 27-81 FAULT TREE 803 FIG. 104 PG. 126 BLOCK 2, THE OVERLOAD INDICATOR WAS RESET. CHECKED ALL RIGHT WING ROTARY ACTUATORS PER MM 27-81-18 FIG 6,
- [SDR FDEA201304190808](https://openairdocs.org/sdr/FDEA201304190808.md): Cover · out of position · Apr 19, 2013 · N940FD · Boeing 757236 · Passenger/Crew Doors
  > WHEN CLOSING AND ARMING, RT DOOR TAB POPS OUT TO INDICATE DOOR IS ARMED APPEARS TO BE BINDING AND DOES NOT POP OUT. FOUND TAB HANGING UP ON DOOR COVERING, TRIMMED COVERING AND PERFORMED OPS CHECK OF SLIDE ARM/DISARM FUNCTION IAW AMM 52-11-20-5. POP OUT TAB
- [SDR FDEA201212214351](https://openairdocs.org/sdr/FDEA201212214351.md): Cover · loose · Dec 21, 2012 · N940FD · Boeing 757236 · Escape Slide
  > L1 DOOR SLIDE COVER LOOSE. SECURED & INSTALLED L1 DOOR SLIDE COVER IAW MM 25-66-01-4. OPS NORMAL.. OK FOR SERVICE.
- [SDR FDEA201210163630](https://openairdocs.org/sdr/FDEA201210163630.md): Cover · unsecure · Oct 16, 2012 · N940FD · Boeing 757236 · Escape Slide
  > BOTH ENTRY DOORS SLIDE COVERS NOT ATTACHED AT BOTTOM. SECURED BOTH ENTRY DOOR SLIDE COVER REF AMM 25-66-01-4.
- [SDR FDEA201203150952](https://openairdocs.org/sdr/FDEA201203150952.md): Lamp · inoperative · Mar 15, 2012 · N940FD · Boeing 757236 · Emergency Lighting
  > DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.
- [SDR FDEA201203080821](https://openairdocs.org/sdr/FDEA201203080821.md): Girt Bar · out of position · Mar 8, 2012 · N940FD · Boeing 757236 · Emergency Equipment
  > R1 DOOR ARMED LIGHT INOPERATIVE. REPOSITIONED GIRT BAR IAW AMM 25-66-10-2-0. OPS CHECKED GOOD.
- [SDR FDEA201202230667](https://openairdocs.org/sdr/FDEA201202230667.md): Target · missing · Feb 23, 2012 · N940FD · Boeing 757236 · Emergency Equipment
  > RT MAIN DOOR ARMING LIGHT WOULD NOT COME ON WHEN DOOR LATCHED SHUT AND GIRTH BAR FELL OUT OF STOWED POSITION. FOUND PROXIMITY SWITCH TARGET ON GIRT BAR NOT INSTALLED, REPOSITIONED TARGET ON GIRT AND INSTALLED GIRT BAR ON DOOR. ADJUSTEMENT CHECKED IAW MM 25-6
- [SDR FDEA201201180240](https://openairdocs.org/sdr/FDEA201201180240.md): Doubler · missing · Jan 18, 2012 · N940FD · Boeing 757236 · Cargo/Baggage Doors
  > FWD LWR CARGO NR1 DOOR INTERNAL SKIN SURFACE FOUND INTERNAL SKIN DOUBLER MISSING IN APPROX (5") AREA AT DOOR UPPER AFT CORNER. REPAIR CARRIED OUT IAW EA F-5230-154463, PART 1 (CARGO DOORS - EXISTING TRIM OUT FOUND ON NR 1 CARGO DOOR ASSY UPPER AFT CORNER OU
- [SDR FDEA201201090048](https://openairdocs.org/sdr/FDEA201201090048.md): Fitting · loose · Jan 9, 2012 · N940FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings
  > NR 1 NACELLE STRUT INBD BATHTUB FITTING MOUNTING BOLTS, FOUND LOOSE. BATHTUB FITTING R & R IAW EA F-5450-154642A.
- [SDR FDEA201201040014](https://openairdocs.org/sdr/FDEA201201040014.md): Skin · damaged · Jan 4, 2012 · N940FD · Boeing 757236 · Leading Edge Devices
  > LT WING NR 5 SLAT FOUND SMALL DRILLED HOLE AT 22" FROM INBD. REPAIRED IAW EA F-5750-157114. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201201030004](https://openairdocs.org/sdr/FDEA201201030004.md): Tie Rod · short · Jan 3, 2012 · N940FD · Boeing 757236 · Buffet/Galleys
  > WHILE CARRYING OUT EO F-2530-7-5000, PT9, STEP 3, GALLEY 1A UPPER CENTER ATTACHING ROD WILL NOT FIT (TOO SHORT). EA F-2530-153492 COMPLIED WITH. THIS ALTERATION IS CLASSIFIED AS MINOR IAW GMM.
- [SDR FDEA201112295455](https://openairdocs.org/sdr/FDEA201112295455.md): Skin · dented · Dec 29, 2011 · N940FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > DENT ON EXTERIOR SKIN AT BS 1690 AT STRINGER 16-17R. DENT REPAIR CARRIED OUT AS PER E.A. F-5330-154485. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112295454](https://openairdocs.org/sdr/FDEA201112295454.md): Web · torn · Dec 29, 2011 · N940FD · Boeing 757236 · Passenger/Crew Doors
  > R4 DOOR, FOUND A TEAR IN DOOR LIGHTNING HOLE BETWEEN 2ND AND 3RD FRAMES. COMPLIED WITH EA F-5210-153486, PART 1. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM.
- [SDR FDEA201112225419](https://openairdocs.org/sdr/FDEA201112225419.md): Floorbeam · corroded · Dec 22, 2011 · N940FD · Boeing 757236 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 324, RBL 38 TO 40 HAS CORROSION ON UPPER TEE. CORROSION FOUND WITHIN SRM LIMITS. REMOVED & REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112215404](https://openairdocs.org/sdr/FDEA201112215404.md): Frame · chafed · Dec 21, 2011 · N940FD · Boeing 757236 · Fuselage Main, Frame
  > AFT LWR CARGO COMP, FRAME AT BS 1520 UPPER SURFACE CHAFED BETWEEN STRINGER 22 & 23R. REPAIR CARRIED OUT ON FRAME AT STA 1520 BETWEEN S-22R AND S-23R IAW EA F-5310-153485. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112215396](https://openairdocs.org/sdr/FDEA201112215396.md): Stringer Fitting · damaged · Dec 21, 2011 · N940FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > AFTER DOUBLER REMOVAL AT BS 1720, FOUND STRINGER END FITTING AT FORWARD SIDE OF BULKHEAD AT STRINGER 29 RT WAS DAMAGED. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112215395](https://openairdocs.org/sdr/FDEA201112215395.md): Stringer Fitting · damaged · Dec 21, 2011 · N940FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > AFTER DOUBLER REMOVAL AT BS 1720, FOUND STRINGER END FITTING AT AFT SIDE OF BULKHEAD AT STRINGER 29 LT WAS DAMAGED. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112215394](https://openairdocs.org/sdr/FDEA201112215394.md): Stringer Fitting · damaged · Dec 21, 2011 · N940FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > AFTER DOUBLER REMOVAL AT BS 1720, FOUND STRINGER END FITTING AT AFT SIDE OF BULKHEAD AT STRINGER 29 RT WAS DAMAGED. STRINGER FITTING R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112215393](https://openairdocs.org/sdr/FDEA201112215393.md): Floorbeam · corroded · Dec 21, 2011 · N940FD · Boeing 757236 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 377, BL 0 TO LBL 45 HAS CORROSION ON UPPER CHORD. CORRODED FLOORBEAM AT STA 377, R & R IAW SRM 51-40-02, REV 104, WITH EA F-5100-1544446 (ALTERNATE ANODIZING METHOD) COMPLIED. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112205374](https://openairdocs.org/sdr/FDEA201112205374.md): Frame · damaged · Dec 20, 2011 · N940FD · Boeing 757236 · Fuselage Main, Frame
  > AFT LWR CARGO COMP, AFTER REMOVAL OF FASTENERS FOUND FRAME BS 1380 HAS ELONGATED HOLE BETWEEN STR 25 & 26R. REPAIR CARRIED OUT IAW EA F-5310-157117. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201112205379](https://openairdocs.org/sdr/FDEA201112205379.md): Stringer Fitting · damaged · Dec 20, 2011 · N940FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > FOUND BS 1720 STRINGER 29L END FITTING AT FORWARD SIDE OF BULKHEAD DAMAGED. END FITTING R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N940FD/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 = 'N940FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N940FD/reports

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