# Service difficulty reports: N942FD

A list on [N942FD](https://openairdocs.org/aircraft/N942FD.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 · 147 reports

- [SDR FDEA202304070595](https://openairdocs.org/sdr/FDEA202304070595.md): Collar · damaged · Apr 7, 2023 · N942FD · Boeing 757200 · Passenger/Crew Doors
  > GUST LOCK BROKEN AT LEFT ENTRY DOOR. PART 07APR23 16:15 GSO U IDENTIFIED PARTS L1 DOOR COLLAR ASSY. REPLACED HOLD OPEN COLLAR AND CATCH. CKS GOOD.
- [SDR FDEA202205281322](https://openairdocs.org/sdr/FDEA202205281322.md): Gust Lock · broken · May 28, 2022 · N942FD · Boeing 757200 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK BROKEN. REMOVED ACCESS PANEL FOR L1 DOOR COLLAR ACCESS, REMOVED BROKEN COLLAR, WHILE TRYING TO INSTALL NEW COLLAR SPLINES WOULD NOT LINE UP SO REORDERED DIFFERENT PART. PAN
- [SDR FDEA202205171235](https://openairdocs.org/sdr/FDEA202205171235.md): Frame · cracked · May 17, 2022 · N942FD · Boeing 757200 · Fuselage Main, Frame
  > DURING OPEN HOLE INSP OF RH STA1640 S-14R. CRACK INDICATION NOTED IN O/B & I/B LOWER HOLES ON THE AFT TWO LAYERS AT 9 O'CLOCK (VIEW LOOKING AFT) COMPLETED & COMPLIED WITH STEPS 1-9 OF EA F-5310-T0368137 PART 1 ON R/H STA. 1640 CRACK INDICATION FINDINGS IN
- [SDR FDEA202105141225](https://openairdocs.org/sdr/FDEA202105141225.md): Gust Lock · broken · May 14, 2021 · N942FD · Boeing 757225 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK INOPERATIVE. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK REF AMM: 52-11-08-8. DOOR HOLD OPEN LOCK OPERATES NORMAL. DOOR HOLD OPEN LOCK MPN 10N0244-7 CPN 5214377 NSN. A/C OK FOR SERVICE.
- [SDR FDEA202103180693](https://openairdocs.org/sdr/FDEA202103180693.md): Relay · failed · Mar 18, 2021 · N942FD · Boeing 757225 · Air Data Computer
  > AT FL370 BEGAN DESCENT TO FL350.GOT IAS DISAGREE, ALT DISAGREE, MACH SPEED TRIM, RUDDER RATIO, L ENG EEC, R ENG EEC EICAS MESSAGES. FOLLOWED CHECKLISTS AND DETERMINED CAPT ADC WAS AT FAULT. SWITCHED TO ALTN SYSTEM. DECLARED AN EMERGENCY AND CONTINUED INTO
- [SDR FDEA202103160669](https://openairdocs.org/sdr/FDEA202103160669.md): Adc · failed · Mar 16, 2021 · N942FD · Boeing 757225 · Air Data Computer
  > ON CLIMBOUT PASSING 38.5 LOST AIRSPEED AND ALTITUDE ON CAPTAINS DISPLAYS-AIR DATA COMPUTER FAILED-ALSO GOT R AND L ENG EEC EICAS, RUDDER RATIO EICAS AND MACH/SPD TRIM EICAS-ELEV ASYM STATUS MGS-COMPLIED WITH QRH. REMOVED AND REPLACED LEFT ADC REF
- [SDR FDEA202012153159](https://openairdocs.org/sdr/FDEA202012153159.md): Gust Lock · inoperative · Dec 15, 2020 · N942FD · Boeing 757225 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK INOP REMOVED AND REPLACED HOLD OPEN LOCK. IN REF TO AMM 52-11-08-4. OPERATIONS CHECKED GOOD. A/C OK TO CONTINUE.
- [SDR FDEA202012153157](https://openairdocs.org/sdr/FDEA202012153157.md): Retainer · dirty · Dec 15, 2020 · N942FD · Boeing 757225 · Emergency Equipment
  > R1 DOOR SLIDE ANNUNCIATOR LIGHT INOPERABLE. GIRT BAR OPERATION NORMAL CLEANED OUT THE GIRT BAR FLOOR RETAINER. LIGHT CHECKS GOOD, PER MM 25-66-00.
- [SDR FDEA202006231323](https://openairdocs.org/sdr/FDEA202006231323.md): Seat Track · corroded · Jun 23, 2020 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN STA 1120-1180 RBL44.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT SEAT TRACK AT STA 1080 - 1180 RBL 44.5, ORIG MAT 0.090", MAT REMOVED 0.038", MAT REMAINING 0.052" OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED, FABRICATED AND INSTALLED SE
- [SDR FDEA2020061971261](https://openairdocs.org/sdr/FDEA2020061971261.md): Butt Joint · corroded · Jun 17, 2020 · N942FD · Boeing 757225 · Fuselage Main, Structure
  > APU INLET AFT BUTTJOINT BS 1825 BETWEEN STRINGERS 3R-6R HAD CORROSION. REMOVED CORROSION ON APU INLET AFT BUTTJOINT IAW SRM 51-10-02. ORIG MAT.100 REM.020 LOSS.080, FOUND OUT OF LIMITS IAW SRM 53-00-01-1A. REPAIRED AREA IAW SRM 53-80-15-2R, REP 1.
- [SDR FDEA2020061621207](https://openairdocs.org/sdr/FDEA2020061621207.md): Seat Track · corroded · Jun 12, 2020 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 900 TO 1180 LBL 58 SEAT TRACK EXFOILATION CORROSION. REMOVED CORR ON SEAT TRACK STA 900 TO 1180 LBL58 IAW SRM 51-10-02. UPON EVAL FOUND OUT OF LIMITS DUE TO EXFOILATION IAW SRM 53-00-52-1A. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW
- [SDR FDEA2020061971148](https://openairdocs.org/sdr/FDEA2020061971148.md): Stringer · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Main, Longeron/Stringer
  > AFT BAY STRINGER 29L BETWEEN BS 1400 TO 1420 CORRODED, REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REPAIR 2, FIG 201, DETAIL III, 51-40-05, 51-40-02, 51-20-01, AMM 51-21-10-7, DWG 146N3110 REV C, BPL 146N3110, REV CB, AND DWG B57-51-001, REV F.
- [SDR FDEA2020061971147](https://openairdocs.org/sdr/FDEA2020061971147.md): Stringer · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY SRINGER 29R BETWEEN STA 1400 TO 1420 CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REP 2, FIG 201, DETAIL III, 53-60-03-01, FIG 1, 51-40-05, 51-40-02, 51-20-01, AMM 51-21-10-7, DWG 146N3110 REV C, PL 146N3110, REV CB, AND DWG B57-5
- [SDR FDEA2020061671145](https://openairdocs.org/sdr/FDEA2020061671145.md): Floor Support · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR SUPPORT STRAP HAS CORROSION AT STA 1020 BETWEEN BL-0 AND RBL-24. REMOVED CORR ON FLOOR SUPPORT STA 1020 BETWEEN BLO AND RBL 24 IAW SRM 51-10-02. ORIG MAT.050 REM.010 LOSS.040 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AN
- [SDR FDEA2020060871144](https://openairdocs.org/sdr/FDEA2020060871144.md): Floor Support · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO BAY LT OF BL0 AT FS 1019 FLOOR STRAP CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 1019 BL0 IAW SRM 51-10-02. ORING MAT.050 REM.020 LOSS.030 OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02, 51-
- [SDR FDEA2020060871148](https://openairdocs.org/sdr/FDEA2020060871148.md): Stringer · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Main, Longeron/Stringer
  > AFT BAY STRINGER 29L BETWEEN STA 1400 TO 1420 CORRODED.
- [SDR FDEA2020060871147](https://openairdocs.org/sdr/FDEA2020060871147.md): Stringer · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER 29R BETWEEN STA 1400 TO 1420 CORRODED.
- [SDR FDEA2020060871145](https://openairdocs.org/sdr/FDEA2020060871145.md): Strap · corroded · Jun 7, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR SUPPORT STRAP HAS CORROSION AT STA 1020 BETWEEN BL-0 AND RBL-24.
- [SDR FDEA202006051133](https://openairdocs.org/sdr/FDEA202006051133.md): Web · damaged · Jun 5, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1635 STR 14R WEB HAS ELONGATED HOLES. UPON EVALUATION FOUND WEB STA 1638 STR 14R TO BE OUT OF LIMITS IAW SRM 51-10- 02. REMOVED, FABRICATED AND INSTALLED NEW WEB IAW DWG 146N8735 REV N AND REV C AND SRM 51-40-02.
- [SDR FDEA2020061241127](https://openairdocs.org/sdr/FDEA2020061241127.md): Repair · delaminated · Jun 4, 2020 · N942FD · Boeing 757225 · Aerodynamic Fairings
  > TAILCONE EXTERIOR LT SIDE HAS A DAMAGED REPAIR. REPAIR AT BS 1960, 8 OCLOCK POSITION. ACCOMPLISHED REPAIR ON TAIL CONE EXTERIOR LT SIDE BS 1960 IAW SRM 53-80-01-2R AND IAW SRM 51-70-10-2R REP 2.
- [SDR FDEA2020060541127](https://openairdocs.org/sdr/FDEA2020060541127.md): Skin · delaminated · Jun 4, 2020 · N942FD · Boeing 757225 · Aerodynamic Fairings
  > TAIL CONE EXTERIOR LT SIDE HAS A DAMAGED REPAIR. REPAIR AT BS 1960, 8 O’CLOCK POSITION.
- [SDR FDEA2020060321113](https://openairdocs.org/sdr/FDEA2020060321113.md): Shear Panel · corroded · Jun 2, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1696 LBL50. REMOVED CORR ON AFT SHEAR DECK STA 1696 LBL50 IAW SRM 51-10-02. ORIG MAT.071 REM.056 LOSS.015 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED DAMAGE IAW SRM 53-60-51-2R REP2 ALT 1.
- [SDR FDEA2020060321112](https://openairdocs.org/sdr/FDEA2020060321112.md): Strap · corroded · Jun 2, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO BAY AT FS 1060 AT LBL 24.75 FLOOR STRAP CORRODED. EVALUATED FLOOR SUPPORT STRAP CRACKED AND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW STRAP IAW DWG 144N5081 REV A AND C AND SRM 51-40-02, 51-40-05 AND 51-40-08.
- [SDR FDEA2020060321111](https://openairdocs.org/sdr/FDEA2020060321111.md): Strap · corrupted · Jun 2, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR SUPPORT STRAP HAS CORROSION AT STA 1017 BETWEEN RBL-24 AND RBL-45. REMOVED CORR ON FLOOR SUPPORT STRAP IAW SRM 51-10-02. UPON REMOVAL OF CORR FOUND TO BE CRACKED AND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW STRA
- [SDR FDEA2020060321109](https://openairdocs.org/sdr/FDEA2020060321109.md): Seat Track · corroded · Jun 2, 2020 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BAY SEAT TRACK AT FS 1200 LBL 24.75 CORRODED. REMOVED CORR ON SEAT TRACK IAW SRM 51-10-02 ORIG MAT.080 REM.042 LOSS.038. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, 51-40-05 AND 51-4
- [SDR FDEA2020061611099](https://openairdocs.org/sdr/FDEA2020061611099.md): Fitting · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO T-CHORD AT LBL-45 HAS CORROSION AROUND MULTIPLE FASTENER HOLES BETWEEN STA 920 AND STA 1040. REMOVED CORR ON T-CHORD STA 900 TO 1040 LBL45 IAW SRM 51-10-02. ORIG MAT.090 REM.070 LOSS.020 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICAT
- [SDR FDEA2020061611097](https://openairdocs.org/sdr/FDEA2020061611097.md): Fitting · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO T-CHORD HAS CORROSION AT RBL-24 BETWEEN STA 1020 AND STA 1040. EVALUATED T-CHORD STA 1020 AND 1040 RBL24 FOUND OUT OF LIMITS 100% MAT LOSS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW T-CHORD IAW SRM 51-40-02 AND DWG 111N5202 REV M AN
- [SDR FDEA2020061011098](https://openairdocs.org/sdr/FDEA2020061011098.md): Crease Beam · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Main, Structure
  > MAIN DECK STA 1605 RBL64.20 CREASE BEAM CORRODED. REMOVED CORROSION FROM MAIN DECK CREASE BEAM STA 1605 RBL 64.20, EVALUATED AREA FOUND OUT OF LIMITS WITH ORIGINAL MATERIAL.070 REMAINING.020, REPIARED AREA OF CREASE BEAM PER SRM 53-00-13-2R REPAIR 1 FIG 2
- [SDR FDEA2020061011102](https://openairdocs.org/sdr/FDEA2020061011102.md): Shear Panel · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1681 LBL39. REMOVED CORR ON AFT SHEAR DECK IAW SRM 51-10-02. ORIG MAT.071 REM.060 LOSS.011 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP 2 ALT 1.
- [SDR FDEA2020061011101](https://openairdocs.org/sdr/FDEA2020061011101.md): Shear Panel · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1688 RBL50. REMOVED CORR ON AFT SHEAR DECK IAW SRM 51-10-02 ORIG MAT.071 REM.058 LOSS.013 OUT OF LIMITS IAW SRM 53-00-51-1A. REPAIRD DAMAGE IAW SRM 53-60-51-2R REP2 ALT 1.
- [SDR FDEA2020061011100](https://openairdocs.org/sdr/FDEA2020061011100.md): Shear Panel · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1681 RBL25 AND RBL33. REMOVED CORR ON SHEAR DECK IAW SRM 51-10-02. ORIG MAT.071 LOWEST.052 RBL25 AND.056 RBL33 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP 2 ALT 1.
- [SDR FDEA2020060111103](https://openairdocs.org/sdr/FDEA2020060111103.md): Intercostal · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION IN THE MAIN CABIN FLOOR STRUCTURE RT CREASE BEAM SUPPORT INTERCOSTAL LOWER SURFACE BS 1615 (VIEW FROM AFT CARGO CEILING AREA). REMOVED CORR ON RT CREASE BEAM SUPPORT INTERCOSTAL STA 1615 IAW SRM 51-10-02. ORIG MAT.050 REM.044 LOSS.006 FOUND TO BE
- [SDR FDEA2020060111100](https://openairdocs.org/sdr/FDEA2020060111100.md): Shear Panel · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1681 RBL25 AND RBL33. REMOVED CORR ON SHEAR DECK STA 1681 RBL25 AND RBL33 IAW SRM 51-10-02. ORIG MAT.071 LOWEST.052 RBL25 AND.056 RBL33 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 531A AND 53-60-51-2R REP 2. REPAIRED AREA IAW
- [SDR FDEA2020060111102](https://openairdocs.org/sdr/FDEA2020060111102.md): Shear Panel · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1681 LBL39. REMOVED CORR ON AFT SHEAR DECK STA 1681 LBL 39 IAW SRM 51-10-02. ORIG MAT.071 REM.060 LOSS.011 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP 2 ALT 1.
- [SDR FDEA2020060111101](https://openairdocs.org/sdr/FDEA2020060111101.md): Shear Panel · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHEAR DECK STA 1688 RBL50. REMOVED CORR ON AFT SHEAR DECK STA 1688 RBL50 IAW SRM 51-10-02 ORIG MAT.071 REM.058 LOSS.013 OUT OF LIMITS IAW SRM 53-00-51-1A. REPAIRD DAMAGE IAW SRM 53-60-51-2R REP2 ALT 1.
- [SDR FDEA2020060111099](https://openairdocs.org/sdr/FDEA2020060111099.md): Tee Fitting · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO T-CHORD AT LBL 45 HAS CORROSION AROUND MULTIPLE FASTENER HOLES BETWEEN STATION 920 AND STATION 1040.
- [SDR FDEA2020060111098](https://openairdocs.org/sdr/FDEA2020060111098.md): Crease Beam · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Main, Structure
  > MAIN DECK STATION 1605, RBL 64.20 CREASE BEAM CORRODED.
- [SDR FDEA2020060111097](https://openairdocs.org/sdr/FDEA2020060111097.md): Tee Fitting · corroded · May 31, 2020 · N942FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CARGO T CHORD HAS CORROSION AT RBL 24 BETWEEN STATION 1020 AND STATION 1040.
- [SDR FDEA201905161086](https://openairdocs.org/sdr/FDEA201905161086.md): Static Line · out of position · May 16, 2019 · N942FD · Boeing 757225 · Emergency Equipment
  > UPON CLOSING THE R DOOR (ENTRY), THE HANDLE WENT IN THE ARMED POSITION, BUT THE ARMED LIGHT WASNT ILLUMINATED. DOOR HANDLE JAMMED IN THE ARMED POSITION. DOOR DIDNT APPEAR TO BE CLOSED AT THE AFT SEAL. ROUTED AND STOWED EXCESS STATIC LINE FROM GIRT BAR TO ESCAP
- [SDR FDEA2019042290861](https://openairdocs.org/sdr/FDEA2019042290861.md): Tire · failed · Apr 19, 2019 · N942FD · Boeing 757225 · Tire
  > #6 TIRE FAILURE ON LANDING COMPLIED WITH TIRE BURST INSP PER AMM 05-51-16. NO DEFECTS NOTED EXCEPT #6 TIRE FAILURE. R&R #6 MLG WHEEL & TIRE ASSY PER AMM 32-45-01. R&R #5 MLG WHEEL & TIRE ASSY PER AMM 32-45-01.
- [SDR FDEA201901220192](https://openairdocs.org/sdr/FDEA201901220192.md): Latch · unlatched · Jan 22, 2019 · N942FD · Boeing 757225 · Passenger/Crew Doors
  > RIGHT ENTRY DOOR LATCH CAME OUT OF LATCHED IN-FLIGHT ON ITS OWN PERFORMED OPS TEST OF R1 DOOR REF MM 52-11-00-2 DOOR CLOSES AND LOCKS WITH NO DEFECTS NOTED INSPECTED DOOR AND FOUND NO VISUAL DEFECTS NO HISTORY FOR 90 DAYS A/C OK FOR SERVICE.
- [SDR FDEA201810283046](https://openairdocs.org/sdr/FDEA201810283046.md): Acm · seized · Oct 28, 2018 · N942FD · Boeing 757225 · Cabin Cooling System
  > ON TAXI OUT, THERE GRINDING NOISE AND SMOKE BELLOWING OUT OF THE GASPERS. THE CREW TURNED OFF THE LEFT PACK AND RAN THE SMOKE AND FIRE, FUMES CHECKLIST. THE SMOKE CLEARED. CFR CHECK OUT THE AIRCRAFT. NO FIRE DETECTED. TAXI BACK TO GATE. COMPLIED WITH SMOKE/FUM
- [SDR FDEA201806221563](https://openairdocs.org/sdr/FDEA201806221563.md): Warning System · false activation · Jun 22, 2018 · N942FD · Boeing 757225 · Central Warning
  > GND PROX SYS FAULT AND BOTH FO PFD AND ND DISPLAYED RED X TERR SYS STATUS MSG ON BLOCK IN. RECYCLED DCU CIRCUIT BREAKER REF AMM 34-22-01-4-99. SYSTEM CHECKS NORMAL.
- [SDR FDEA201806051393](https://openairdocs.org/sdr/FDEA201806051393.md): Skin · debonded · Jun 5, 2018 · N942FD · Boeing 757225 · Trailing Edge Flaps
  > RT INBD FWD FLAP UPPER SURFACE HAS A DISBONDED COMPOSITE REPAIR. REPAIRED RT INBD FWD FLAP UPPER SURFACE IAW SRM 51-71-10-2R REPAIR 4 & 57-53-01-2R FIG 201 DET I.
- [SDR FDEA2018053141315](https://openairdocs.org/sdr/FDEA2018053141315.md): Skin · damaged · May 24, 2018 · N942FD · Boeing 757225 · Fuselage Main, Plate/Skin
  > SKIN DAMAGED, BS 1500 AND 1560, STRINGERS 1L AND 2L. REPAIRED IAW EA F-2560-T0339100, B P2.
- [SDR FDEA201709122478](https://openairdocs.org/sdr/FDEA201709122478.md): Bulb · inoperative · Sep 12, 2017 · N942FD · Boeing 757225 · Emergency Lighting
  > L1 DOOR EMERGENCY SLIDE LIGHT (EXTERIOR) INOPERATIVE. REMOVED BULB AND CLEANED SOCKET. INSTALLED A NEW BULB IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.
- [SDR FDEA201705021340](https://openairdocs.org/sdr/FDEA201705021340.md): Pivot · cracked · May 2, 2017 · N942FD · Boeing 757225 · Main Landing Gear
  > LEFT MAIN LANDING GEAR BEAM RETRACT ACTUATOR LINK PIVOT SHAFT AFT END HAS CIRCUMFERENTIAL CRACKED. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR BEAM RETRACT ACTUATOR LINK PIVOT SHAFT, REFERENCE 32-32-01-4
- [SDR FDEA201704261274](https://openairdocs.org/sdr/FDEA201704261274.md): Actuator · inoperative · Apr 26, 2017 · N942FD · Boeing 757225 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, THE GEAR WOUILD NOT RETRACT PASSED THE OFF POSITION. RAN CHECKLIST, THE GEAR REMAINED DOWN WITH DOOR AND DISAGREE LIGHT LUMINATED SO WE PUT THE GEAR DOWN, GOT NORMAL INDICATION AND LANDED SAFELY. R & R THE LT MLG TRUCK POSITION AC
- [SDR FDEA201702030389](https://openairdocs.org/sdr/FDEA201702030389.md): Girt Bar · obstructed · Feb 3, 2017 · N942FD · Boeing 757225 · Emergency Equipment
  > LT PASSENGER DOOR SLIDE WILL NOT ARM. CLEANED DEBREE FROM GIRT BAR AREA AND TESTED DOOR IAW MM 52-11-25-5-0. CHECKED AND ARMS GOOD.
- [SDR FDEA201612084364](https://openairdocs.org/sdr/FDEA201612084364.md): Harness · defective · Dec 8, 2016 · N942FD · Boeing 757225 · Flight Compartment Equipment
  > F/O RIGHT SHOULDER HARNESS DOES NOT RETRACT. REPLACED F/O SEAT IAW MM 25-11-01-2. OPS CHECKED NORMAL. OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N942FD/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 = 'N942FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N942FD/reports

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