# Service difficulty reports: N922FD

A list on [N922FD](https://openairdocs.org/aircraft/N922FD.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 4 · 195 reports

- [SDR FDEA202407211036](https://openairdocs.org/sdr/FDEA202407211036.md): Battery Pack · no test · Jul 21, 2024 · N922FD · Boeing 75723A · Emergency Lighting
  > ON SERVICE CHECK FOUND EMERGENCY EXIT AISLE SIGN NOT ILLUMINATING WHEN EMERGENCY LIGHTS TEST PERFORMED. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK AS PER 757 AMM 33-51-07-2-0. OPS CHECK GOOD. AIRCRAFT OK FOR SER
- [SDR FDEA202404010430](https://openairdocs.org/sdr/FDEA202404010430.md): Skin · corroded · Apr 1, 2024 · N922FD · Boeing 75723A · Wing, Plate/Skin
  > R / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN CORROSION R/H WING LOWER DRY BAY PANEL REPAIR AT ACCESS PANEL CUTOUT 644 AB, WS 775-806 WITH NO DEV
- [SDR FDEA202403290410](https://openairdocs.org/sdr/FDEA202403290410.md): Web · corroded · Mar 29, 2024 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT F. STA BETWEEN 600-620 RBL 64.5 SHEAR WEB HAS CORROSION AFTER EVALUATED SHEAR WEB AT F.STA 600 TO 620 AND BTW RBL 62.89 - 64.5 FOUND OUT OF LIMITS IAW B-757 SRM 53-30-13-1A FIG 101 DETAIL III; REMOVED, FABRICATED AND INS
- [SDR FDEA202403290408](https://openairdocs.org/sdr/FDEA202403290408.md): Fairing · gouged · Mar 29, 2024 · N922FD · Boeing 75723A · Aerodynamic Fairings
  > SEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-03 AND AFTER EVALUATION TWO DIFERENT AREAS FOUND # 1 AREA AT STA 1862 TO STA 1865 FOUND WITHI
- [SDR FDEA202403280399](https://openairdocs.org/sdr/FDEA202403280399.md): Seat Track · corroded · Mar 28, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL45.50 REMOVED CORROSION AT SEAT TRACK FLANGE BETWEEN STA. 1180-1200 RBL 45.50, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG. 101 DETAIL VIII REMOVED AND INSTALLED NEW SEAT
- [SDR FDEA202403270388](https://openairdocs.org/sdr/FDEA202403270388.md): Seat Track · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS EVIDENCE OF CORROSION ALONG FLANGE UNDER CRACKED PAINT BETWEEN STA 1320-1420 RBL-44 REMOVED CORROSION AT SEAT TRACK I\B FLANGE BETWEEN STA 1320-1420 RBL44 IAW B757 SRM 51-10-02-0G, EVALUATED AREAS FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00
- [SDR FDEA202403270387](https://openairdocs.org/sdr/FDEA202403270387.md): Seat Track · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL 24.75 REMOVED CORROSION AT SEAT TRAK BEWEEN STA 1180-1200 RBL 24.75 IAW B757 SRM 51-10-02- OG, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL VIII, REMOVED AND INST
- [SDR FDEA202403270386](https://openairdocs.org/sdr/FDEA202403270386.md): Seat Track · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE BETWEEN STA 1100-1180 RBL-45.5 REMOVED CORROSION AT SEAT TRACK STA 1075-1180, RBL 455 IAW B757 SRM 51-10-02-0G, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG 101, DETAIL VIII. REMOVED AND REPLACED NEW
- [SDR FDEA202403270385](https://openairdocs.org/sdr/FDEA202403270385.md): Seat Track · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, BETWEEN STA 1100-1180 RBL-24.5 REMOVED CORROSION AFT FLANGE SEAT TRACK A STA 1075-1180 RBL 24.5 IAW B57 SRM 51-10-02- 0G, FOUND TO BE OUT OF LIMTIS IAW B757 SRM 53-00-52-1A DETAIL VIII REMOVED AND INSTALLED NEW SEAT TRACK SE
- [SDR FDEA202403270384](https://openairdocs.org/sdr/FDEA202403270384.md): Crease Beam · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > MAIN DECK, RIGHT CREASE BEAM HAS CORROSION BETWEEN STA.1260-1280. REMOVED CORROSION CREASE BEAM AT STA 1260 TO 1280 IAW B757 SRM 51-10-02-0G, EVALUATED AREA FOUND TO BE OUT OF LIMTIS BETWEEN STA 1260-1280 IAW B757 SRM 53-60-13- 1A DETAIL VIII FIG 101, REPAI
- [SDR FDEA202403270383](https://openairdocs.org/sdr/FDEA202403270383.md): Crease Beam · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > LH AFT MAIN CABIN CREASE BEAM HAS POSSIBLE CORROSION BETWEEN BS 1420 THRU BS 1640 REMOVED CORROSION AT CREASE BEAM BETWEEN STA. 1520 - 1605 IAW B757 SRM 51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-60-13-1A DETAIL VIII, REMOVED AND IINSTALLED NEW
- [SDR FDEA202403260380](https://openairdocs.org/sdr/FDEA202403260380.md): Seat Track · corroded · Mar 26, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, BETWEEN STA 1320-1340, RBL-57 REMOVED CORROSION IAW B757 SRM 51-10-02-0G, NO LIMITS REPLACEMENT REQ. IAW B757 SRM 53-00-52-1A FIG 101 REMOVED AND INSTALLED NEW SEAT TRACK SECTION BETWEEN STA 1180 TO STA 1420 RBL58.22 IAW B75
- [SDR FDEA202403260375](https://openairdocs.org/sdr/FDEA202403260375.md): Angle · corroded · Mar 26, 2024 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARATMENT ON STA 1440 S-27 R\H CLIP ANGLE CORRODED. REMOVED, EVALUATED FOUND OUT OF LIMTIS, FABRICATE, TREATED, PRIMED, TOP COAT AND INSTALLED AFT CRG COMPARTMENT CLIP ANGLE P\N: 146N5422-4 AT STA 1440 S-27 R\H IAW B757 SRMS 51-40-02-0G, 51-2
- [SDR FDEA202403250371](https://openairdocs.org/sdr/FDEA202403250371.md): Bracket · corroded · Mar 25, 2024 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT F.STA 1440 S.27 R BRAKET SUPPOR CORRODED REMOVED, INSPECTED FOUND OUT OF LIMIT, FABRICATED, TREATED, PRIMED TOP COATED AND INSTALLED AFT CRG COMPARTMENT BRAKET P/N 146N8815-1 AT STA 1440 S.27 RH IAW EA F-5320- T0378505, B757 SRM 51-40-
- [SDR FDEA202403250370](https://openairdocs.org/sdr/FDEA202403250370.md): Crease Beam · corroded · Mar 25, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > MAIN DECK RIGHT SIDE CREASE BEAM, HAS CORROSION BETWEEN STA 1580-1620. REMOVED CORROSION ON CREASE BEAM IAW B757 SRM 51-10-02-0G FOUND TO BE OUT OF LIMITS AT AREA BETWEEN STA 1583-1603 RBL 64.20, IAW B757 SRM 53-60-13-1A FIG 101 DETAIL VIII, REPAIR CREASE
- [SDR FDEA202403240359](https://openairdocs.org/sdr/FDEA202403240359.md): Seat Track · worn · Mar 24, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, FOUND SEAT TRACK DAMAGED ON CROWN AREAS STA 1580 RBL 24.75. REWORKED DAMAGED AREAS AT SEAT TRACK CROWN AREA AT BETWEEN STA 1570-1590 RBL 24.5 IAW B757 SRM 51-10-02-0G, AREA FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL 1,
- [SDR FDEA202403240358](https://openairdocs.org/sdr/FDEA202403240358.md): Seat Track · corroded · Mar 24, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE BETWEEN STA 1320-1340, RBL-57.
- [SDR FDEA202403220350](https://openairdocs.org/sdr/FDEA202403220350.md): Seat Track · corroded · Mar 22, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT BETWEEN F. STA 1280-1300 RBL 45.50 SEAT TRACK HAVE CORROSION REMOVED CORROSION AT SEAT TRACK SECTION BETWEEN STA. 1280-1300 RBL 45.50 IAW B757 SRM 51-10-02-0G, BLENDED AREA FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A DETAIL VII
- [SDR FDEA202403220349](https://openairdocs.org/sdr/FDEA202403220349.md): Seat Track · corroded · Mar 22, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK,SEAT TRACK HAS CORROSION AT FLANGE, STA 1537 RBL-57 REMOVED CORROSION AT SEAT TRACK I/B FLANGE IAW B757 SRM 51-10-02-0G, AREA NO LIMITS IAW B757 SRM 53-60-52-01 DETAIL II REMOVED AND INSTALLED NEW SEAT TRACK SECTION, BETWEEN STA 1420 TO STA 1620
- [SDR FDEA202403220348](https://openairdocs.org/sdr/FDEA202403220348.md): Seat Track · corroded · Mar 22, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION, ON LOWER SURFACE OF CLIPS NUTS HOLES, BETWEEN STA/ 1300 - 1320, RBL24.5 REMOVED CORROSION AT SEAT TRACK SECTION BETWEEN STA/ 1300-1320, RBL24.75 IAW B757 SRM 51-10-02-06, BLENDED AREA FOUND OUT LIMITS IAW B757 SRM 53-00-52-1A DE
- [SDR FDEA202403220347](https://openairdocs.org/sdr/FDEA202403220347.md): Floor Support · corroded · Mar 22, 2024 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > REWORK REQUIRED ON NR# N00383 FOR NOT PERFORMING REQUIRED HARDNESS TEST FOR FLOOR SUPPORT LOCATED AT STA 339 LBL 60. PERFORMED REQUIRE HARDNESS TEST ON FABRICATED FLOOR SUPPORT P\N: 141N5170-39 LOCATED AT STA 339 LBL 60. MATERIAL 7075-T6 0.050" IAW B757 S
- [SDR FDEA202403210336](https://openairdocs.org/sdr/FDEA202403210336.md): Deck Plate · gouged · Mar 21, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > MAIN CABIN AFT DECK PLATE FOUND GOUGE OUT OF LIMITS AT STA 1682 LBL 7. REPAIRED AREA OUT OF LIMITS ON DECK PLATE AT STA. 1682 LBL 7 IAW B-757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I FIG. 201. MAJOR REPAIR.
- [SDR FDEA202403210335](https://openairdocs.org/sdr/FDEA202403210335.md): Deck Plate · gouged · Mar 21, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > MAIN CABIN AFT DECK PLATE FOUND GOUGE OUT OF LIMITS AT STA 1711, LBL 7. REPAIRED AREA OUT OF LIMITS ON DECK PLATE AT STA 1711 LBL 7 IAW B-757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I FIG. 201. MAJOR REPAIR
- [SDR FDEA202403210334](https://openairdocs.org/sdr/FDEA202403210334.md): Crease Beam · corroded · Mar 21, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > R/H MAIN CABIN CREASE BEAM HAS CORROSION BETWEEN BS 840 THRU BS 880. MAIN CABIN CREASE BEAM BETWEEN BS 733-900 REMOVED CORROSION IAW B757 SRM 51-10-02- 0G, FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-30-13-1A DETIAL VIII, REMOVED AND REPLACED SECTION CREASE B
- [SDR FDEA202403170305](https://openairdocs.org/sdr/FDEA202403170305.md): Seat Track · corroded · Mar 17, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 1195 LBL-26. AFTER EVALUATED CORROSION AREA ON SEAT TRACK FLANGE AT STA. 1195, LBL 26 FOUND OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 SHEET 4 DETAIL VIII, REMOVED AND REPLACED SEAT TRACK SECTION AT STA. 1180 TO 1240
- [SDR FDEA202403170304](https://openairdocs.org/sdr/FDEA202403170304.md): Seat Track · corroded · Mar 17, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION, AT STA 1427 RBL-25. AFTER EVALUATED CORROSION AREA ON SEAT TRACK STA 1427 RBL25 FOUND OUT OF LIMTIS IAW B757 SRM 53-00-51-1A FIG 101 SHEET 4 DETAIL VIII & I, REMOVED AND REPLACED SEAT TRACK SECTION, STA 1320 TO 1540 RBL 24.75 IAW
- [SDR FDEA202403150293](https://openairdocs.org/sdr/FDEA202403150293.md): Crease Beam · corroded · Mar 15, 2024 · N922FD · Boeing 75723A · Fuselage Main, Structure
  > CREASE BEAM HAS CORROSION, BETWEEN STA 1320-1350 NEXT TO R-3 DOOR. REMOVED CORROSION IAW B757 SRM 51-10-02-0G AT CHORD, OUT OF LIMTIS IAW B757 SRM 53-60- 13-1A DETAIL VIII, REMOVED AND REPLACED CHORD ON R\H STA 1300 TO 1400 RBL 64. IAW B757 SRM 51-40-02-0G
- [SDR FDEA202403120278](https://openairdocs.org/sdr/FDEA202403120278.md): Floor Support · corroded · Mar 12, 2024 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > L-1 ENTRY DOOR UPPER SIDE OF THE FLOOR SUPPORT AT STA 339 LBL 60 FOUND CORROSION. REMOVED CORROSION AT L-1 ENTRY DOOR STA 339 LBL 60 ON FLOOR SUPPORT IAW B757 SRM 51-10-02-0G, OUT OF LIMITS IAW B757 SRM 53-10-15-1A DETAIL IV FIG 101, REMOVED AND INSTALLED
- [SDR FDEA202402130160](https://openairdocs.org/sdr/FDEA202402130160.md): Unknown · odor · Feb 13, 2024 · N922FD · Boeing 75723A · Air Distribution System
  > AT GATE, STATUS MESSAGES EQT CLG TEST AND WARN ELEX APPEARED, AT THE SAME TIME A STRONG FOUL RUBBER/ELECTRICAL ODOR PRESENTED ITSELF. EQUIPMENT COOLING SYSTEM TEST C/O NORMAL IAW FIM 21-58 FAULT TREE 912 133.3 NO FUMES OBSERVED/SMELLED
- [SDR FDEA202310271801](https://openairdocs.org/sdr/FDEA202310271801.md): Container · failed · Oct 27, 2023 · N922FD · Boeing 757200 · Emergency Equipment
  > POB AT COURIER AREA FOUND DAMAGE (PROTECTIVE BAG LOST VACUUM) PROTECTIVE BREATHING EQUIPMENT, NOT POB MEL 27OCT23 07:49 BCN U RELEASED FOR SERVICE PER MEL: 35-20-01 CATEGORY: D EXPIRATION: 24FEB24 "MEL 35-20-01: COURIER COMPARTMENT PBE UNIT - REMOV
- [SDR FDEA202304240757](https://openairdocs.org/sdr/FDEA202304240757.md): Panel · delaminated · Apr 24, 2023 · N922FD · Boeing 757200 · Horizontal Stabilizer Structure
  > DURING OPEN UP FOR ELEVATOR LUBRICATION FOUND ACCESS PANEL 345BB EDGE DELEMINATED PERFORMED WET LAYUP REPAIR FOR MENTIONED PANEL PER SRM 51-70-17,PAR. 4.G. REF. SRM 55-10-01-2R, REP.5, FIG. 201,TABLE II. REP. DIM.: 4" X 2.5", REP. LOC.: 2" FROM I/B EDGE
- [SDR FDEA202212072888](https://openairdocs.org/sdr/FDEA202212072888.md): Exhaust Valve · stuck · Dec 7, 2022 · N922FD · Boeing 757200 · Cabin Pressure Control System
  > PDIS 922 21-30 3695 07DEC22 CDG FACT U RECEIVED CABIN ALT WARNING IN FLIGHT AT FL400. CABIN ALT WAS JUST OVER 10,000. DIFFERENTIAL PRESSURE WAS APPROXIMATELY 7PSI. WE DESCENDED TO 10,000. EXECUTED THE QRC/QRH. WE KEPT THE CABIN ALTITUDE
- [SDR FDEA202211172814](https://openairdocs.org/sdr/FDEA202211172814.md): Control Panel · failed · Nov 17, 2022 · N922FD · Boeing 75723A · Fire Detection
  > JUST PRIOR TO TOP OF DESCENT, RECEIVED A FIRE LOOK UP LIGHT WITH ALL MAIN CARGO FIRE INDICATORS ILLUMINATED. QRH COMPLETED & AN EMERGENCY DECLARED. THERMO IMAGED THE ENTIRE AIRCRAFT AND OBSERVED NO SIGNS OF FIRE. AMM 26-16-98-4-0 DURING INSPECTION, FOU
- [SDR FDEA202210272677](https://openairdocs.org/sdr/FDEA202210272677.md): Oil System · low pressure · Oct 27, 2022 · N922FD · Boeing 75723A · APU Oil System
  > APU SHUTDOWN AT CRUISE RESULTING IN SINGLE GENERATOR REMAINING. EMERGENCY DECLARED AND RETURNED TO LFPG FOR NORMAL LANDING. EMERGENCY DECLARED, APU SHUT DOWN IS RELATED TO WRI 49-90/3559 WITH CORRECTIVE ACTION, APU OIL QTY IN STATUS, SUDDEN APU OIL
- [SDR FDEA202208071945](https://openairdocs.org/sdr/FDEA202208071945.md): Sensor · loose · Aug 7, 2022 · N922FD · Boeing 757200 · Emergency Exits
  > PDIS 922 52-20 3302 07AUG22 MEM FACT U L EMER DOOR EICAS MESSAGE AFTER POWER TRANSFER T/S REF. B757 FIM 52-71 FT 802/805, NO FAULT CODES NOTED. TARGET TEST FAR WITH DOOR CLOSED, FOUND SENSOR LOOSE. SECURED SENSOR REF. B757 AMM 52-71-00-5-0,
- [SDR FDEA202208061944](https://openairdocs.org/sdr/FDEA202208061944.md): Target · faulted · Aug 6, 2022 · N922FD · Boeing 757200 · Emergency Exits
  > PDIS 922 52-20 3299 06AUG22 MEM FACT U L EMER DOOR EICAS MESSAGE DISPLAYED CLIMBING THROUGH 9,500 MSL. CAIN DIFFERENTIAL WAS 4.4 AND CABIN ALTITUDE WAS 800 FEET. REMAINED ILLUMINATED UNTIL 800 FEET AGL ON FINAL APPROACH THEN EICAS MESSAGE EX
- [SDR FDEA202208041888](https://openairdocs.org/sdr/FDEA202208041888.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #15. #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV. E PART 1, CAT B AND MAJOR
- [SDR FDEA202208041887](https://openairdocs.org/sdr/FDEA202208041887.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #9 #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 10. TITLE: WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-0340076 REV E PART 1, CAT B AND MAJOR REP
- [SDR FDEA202208041886](https://openairdocs.org/sdr/FDEA202208041886.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #8. #1 PYLON FITTING PERFORMED REAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23. TITLE: WINGS-PLATES AND SKINS- LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PT1, CAT B AND MAJO
- [SDR FDEA202208041885](https://openairdocs.org/sdr/FDEA202208041885.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE INDICATINS NOTED IN HOLE #4 #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23, TITLE: WINGS-PLATES AND SKINS-LH WING-UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PT1, CAT B MAJOR REPA
- [SDR FDEA202208041884](https://openairdocs.org/sdr/FDEA202208041884.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #3 #1 PYLON FITTING. PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 21, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PART 1, FITTING REPLACED ON N/R
- [SDR FDEA202208041882](https://openairdocs.org/sdr/FDEA202208041882.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE NOTED ON HOLE #3 #2 PYLON PERFORMED REPAIR ON E.A. F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX E.O. F-5730-E0340076 REV. E P2) STEP #9, CAT B AND MAJOR REPAIR
- [SDR FDEA202208041878](https://openairdocs.org/sdr/FDEA202208041878.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE NOTED ON HOLE #4 #2 PYLON PERFORMED REPAIR ON EA F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING,UPPER SKIN AT DRAG FITTING, CORROSION REPAIR;FEDEX EO F-5730-E0340076 REV. E P2) STEP #4, CAT B AND MAJOR REPAIR.
- [SDR FDEA202208041877](https://openairdocs.org/sdr/FDEA202208041877.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > REJECTABLE DAMAGE NOTED ON HOLE #6 #2 PYLON PERFORMED REPAIR ON E.A. F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING,CORROSION REPAIR-FEDEX E.O. F-5730-E0340076 REV. E P2) STEP #9, CAT B AND MAJOR REPAIR.
- [SDR FDEA202208041876](https://openairdocs.org/sdr/FDEA202208041876.md): Skin · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON INBD. FITTING #12 HOLE DAMAGED IN SKIN ONLY PERFORMED REPAIR ON EA F-5730-T0361920 PT STEP 10, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX E.O. F-5730-E0340076 REV. E PART 1, CAT B AND MAJOR REPAIR.
- [SDR FDEA202208041880](https://openairdocs.org/sdr/FDEA202208041880.md): Drag Fitting · cracked · Aug 4, 2022 · N922FD · Boeing 757200 · Wing, Attach Fittings
  > REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #4, #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 PT1 STEP 20 AND 23. TITLE: WINGS - PLATES AND SKINS - LH WING - UPPER SKIN AT DRAG FITTING CORROSION REPAIR - FED EX EO F-5730- E0340076 REV E PT 1. MAJ
- [SDR FDEA202208031856](https://openairdocs.org/sdr/FDEA202208031856.md): Drag Fitting · cracked · Aug 3, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Attach Fittings
  > REJECTABLE DAMAGE NOTED ON HOLE #12.593, #2 PYLON THRU SKIN AND FITTING TITLE-WINGS-PLATES AND SKINS-RH WING UPPER SKIN @ DRAG FITTING, CORROSION REPAIR- FEDEX E.O. F-5730-E0340076 REV. E PART 2, IS COMPLIED WITH STEP #9 ON FINAL EA # F-5730- T0369270 P1, M
- [SDR FDEA202208031850](https://openairdocs.org/sdr/FDEA202208031850.md): Drag Fitting · cracked · Aug 3, 2022 · N922FD · Boeing 757200 · Nacelle/Pylon, Attach Fittings
  > REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #10 #1 PYLON FITTING. PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 10, WINGS-PLATES AND SKIN-LH WING, UPPER SKIN @ DRAG FITTING CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PART 1 BY REPLACED OB DRAG FITTING
- [SDR FDEA202108172021](https://openairdocs.org/sdr/FDEA202108172021.md): Light · inoperative · Aug 17, 2021 · N922FD · Boeing 75723A · Emergency Lighting
  > MDIS 922 33-50 2242 13AUG21 CDG FACT U FOUND L1 EMER DOOR GROUND ILLUMINATION LIGHT INOP. SHGN 13AUG21 19:28 CDG U RELAMPED AS PER MM:33-51-06-2-1. LIGHT TEST OK. DURING L1 EMER LIGHT LENS REINSTALLATION, FOUND 4 SCREWS WORN AND UNABLE TO
- [SDR FDEA202107271872](https://openairdocs.org/sdr/FDEA202107271872.md): Door · cracked · Jul 27, 2021 · N922FD · Boeing 75723A · Landing Gear Doors
  > LMG BODY DOOR CRACKED AFT OF TANG REPAIRED LMG DOOR CRACKED AFT OF TANG IAW FEDEX B757 SRM: 52-80-02, 51-70-06-0G, DWG #149N6003 AND AMM 51-21-00. MINOR REPAIR

Next page: https://openairdocs.org/aircraft/N922FD/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 = 'N922FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N922FD/reports

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