# Service difficulty reports: N773FD

A list on [N773FD](https://openairdocs.org/aircraft/N773FD.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 · 110 reports

- [SDR FDEA202502050179](https://openairdocs.org/sdr/FDEA202502050179.md): Floor Panel · damaged · Feb 5, 2025 · N773FD · Boeing 757222 · Fuselage Floor Panel
  > VERIFY AFT R/H FLOOR PNL 252MWF HAS THE WRONG INSERTS INSTALLED AND HAS MISSING INSERTS AND HAS COMPOSITE DAMAGE THE ENTIRE LENGTH FABRICATED FLOOR PANEL 252MWF ON VTMAE TRAVELER #T25/1798171 IAW VTMAE DWG #11864182-49, MAJOR REPAIR
- [SDR FDEA202406290903](https://openairdocs.org/sdr/FDEA202406290903.md): Girt Bar · dislodged · Jun 29, 2024 · N773FD · Boeing 757222 · Emergency Equipment
  > L1 DOOR UNABLE TO ARM PRIOR TO PUSH. GIRT BAR DISLODGED POSITIONED & RECONNECTED L1 DR GIRT BAR REF AMM 25-66-10-2. FUNCTIONAL CHK GOOD, INDCN NORMAL. NO OTHER FAULTS NOTED. ITEM CLOSED. A/C OK TO CONTINUE.
- [SDR FDEA202312051916](https://openairdocs.org/sdr/FDEA202312051916.md): Rod End · sheared · Dec 5, 2023 · N773FD · Boeing 757200 · Passenger/Crew Doors
  > R1 DOOR, ROD END BROKEN AT LOWER DOOR HINGE. COMPLIED WITH E.A. F-5210-T0377325 PART 1. DOOR VERIFIED CLOSED, LOCKED AND SECURED FROM INSIDE AND OUTSIDE. PLACED OLD R1 SLEEVE AND ADJUSTER IN LABLED BOX IN GALLEY AREA. RELEASED FOR SERVICE PER MEL: 52-11-
- [SDR FDEA202309221636](https://openairdocs.org/sdr/FDEA202309221636.md): Unknown · unknown · Sep 22, 2023 · N773FD · Boeing 757200 · Electrical Power System
  > ON TAKE OFF ROLL 110KT, CIRS DC, ATC FAULT CAUTION. AFTER ROTATION ALT CALL OUTS, GND PROX SYS, EQPT OVHT CAUTION. LT AFT FUEL PUMP, RT FWD FUEL PUMP CAUTION BELOW 3000 FT. RETURNED TO FIELD. ON LANDING, ELECT SYS CIRCUIT EQPT COOLING FAN, FWD FUEL BOOST PUM
- [SDR FDEA202304190704](https://openairdocs.org/sdr/FDEA202304190704.md): Unknown · cracked · Apr 19, 2023 · N773FD · Boeing 757200 · Fuselage Structure (General)
  > AFT CARGO DOOR LOWER SILL FWD CORNER LOWER CHORD IS CRACKED. ALL STEPS COMPLIED WITH IAW EA TF-5310-T0313798 FUSELAGE / MAIN FRAME - EXISTING REPAIR AT FUSELAGE NO 2 CARGO DOORWAY LOWER MAIN OUTBOARD CHORD BETWEEN BS 1380 TO BS 1436 MAJOR REPAIR
- [SDR FDEA202303240501](https://openairdocs.org/sdr/FDEA202303240501.md): Fitting · worn · Mar 24, 2023 · N773FD · Boeing 757200 · Wing, Plate/Skin
  > LH WING LWR ATTACHING FITTING COMMON TO I/B DRAG FITTING HAVE 3 HOLES WITH DAMAGE & OUT ROUND CONDITION. I/B DRAG FITTING HAVE 2 HOLES WITH DAMAGE AND OUT ROUND CONDITION. MARKED IN RED. REPAIR BEFORE NDT INSP. COMPLIED WITH EA # F - 5740-T0373064 P1. TITL
- [SDR FDEA202303240500](https://openairdocs.org/sdr/FDEA202303240500.md): Fitting · corroded · Mar 24, 2023 · N773FD · Boeing 757200 · Nacelle/Pylon Structure
  > DURING ROTO -TEST OF HOLES 3 AND 8 OF THE L/H WING NDT RECEIVED CORROSION INDICATIONS DOCUMENTED ON F-5730-E0340076 P1, JPF STEP 7. COMPLIED WITH EA # F-5740-T0373064 P1. TITLE: WINGS - ATTACH FITTINGS - LH WING, UPPER SKIN, DRAG FITTINGS, CRACK INDICATION
- [SDR FDEA202303140425](https://openairdocs.org/sdr/FDEA202303140425.md): Floorboard · cracked · Mar 14, 2023 · N773FD · Boeing 757200 · Fuselage Main, Structure
  > MDCC FLOOR PANEL 251MXF CRACKED/BROKEN. FABRICATED MDCC FLOOR PANEL 251MXF ON VTMAE TRAVELER # T23/1663103 IAW DWG SRZ-25- 005 REVISION R. MAJOR REPAIR
- [SDR FDEA202202040233](https://openairdocs.org/sdr/FDEA202202040233.md): Pressure Switch · failed · Feb 4, 2022 · N773FD · Boeing 757200 · Fuel Boost Pump
  > JUST PRIOR TO LEVEL OFF, RECEIVED L CTR FUEL PUMP EICAS MESSAGE. COMPLIED WITH QRH. WITH MEL 28-22-02-A ALREADY ON AIRCRAFT FOR RIGHT CENTER PUMP, WE DID NOT HAVE SUFFICIENT FUEL TO CONTINUE TO DESTINATION. DIVERTED TO KMCI PER GOC REQUEST. UPON F
- [SDR FDEA202108182031](https://openairdocs.org/sdr/FDEA202108182031.md): Actuator · faulted · Aug 18, 2021 · N773FD · Boeing 757222 · Leading Edge Slat Actuator
  > ON CLIMB OUT GOT EICAS MESSAGE LE SLAT DISAGREE AND LEADING EDGE DISCRETE LIGHT RETRACTING THE FLAPS AT 200 KNOTS AND 3000 FEET QRH COMPLIED WITH. TROUBLESHOT PER B757 FIM 27-81 FAULT TREE 803 AND FOUND OVERLOAD INDICATOR TRIPPED ON THE INBD SLAT PDU TORQUE L
- [SDR FDEA202105281417](https://openairdocs.org/sdr/FDEA202105281417.md): Circuit Card · faulted · May 28, 2021 · N773FD · Boeing 757222 · Fire Detection
  > FWD CARGO DET 1 EICAS MESSAGE REPLACED AFOLTS CARD M10427 CARGO TESTS NORMAL REF M.M. 26-10-01-4.
- [SDR FDEA202103170683](https://openairdocs.org/sdr/FDEA202103170683.md): Rib · cracked · Mar 17, 2021 · N773FD · Boeing 757222 · Wing, Rib/Bulkhead
  > LH FIXED WING L/E O/B OF PYLON BULL NOSE ATTACHMENT BRACKET HAS 2EA CRACKS AT FASTENER HOLES REPAIRED PER EA #F-5710-T0360377-P1 WINGS-BASIC WING STRUCTURE -L/H WING,OUTBOARD FIXED LEADING EDGE,OSS 305,CLOSURE RIB,CRACKED FASTENER HOLES
- [SDR FDEA202103160671](https://openairdocs.org/sdr/FDEA202103160671.md): Tee Fitting · damaged · Mar 16, 2021 · N773FD · Boeing 757222 · Fuselage Main, Attach Fittings
  > TEE CLIP COMMON TO STA 1640 FUSELAGE FRAME WEB AND STRINGER S-14L SHOWS 2 EA REJECTABLE INDICATIONS ON ON UPPER AND LOWER INBOARD HOLES. POSSIBLE TOOLING DAMAGE. UPPER INB HOLE INDICATION APX 1 O'CLOCK POSITION. POSITION. LOWER INB HOLE INDICATION APX AT TH
- [SDR FDEA202103130635](https://openairdocs.org/sdr/FDEA202103130635.md): Web · cracked · Mar 13, 2021 · N773FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > R1 DOOR CUTOUT, HINGE BOX, INBOARD WEB IS CRACKED REMOVED, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 141N8415 AND DWG 141N8441
- [SDR FDEA202103130636](https://openairdocs.org/sdr/FDEA202103130636.md): Doubler · cracked · Mar 13, 2021 · N773FD · Boeing 757222 · Fuselage, Door Hinge
  > MAIN CABIN L2 DOOR FWD UPPER HINGE REPAIR DOUBLER IS CRACKED ACCOMPLISHED FEWDEX EA# F-5210-T0315976: DOORS-PASSENGER/CREW - EXISTING REPAIR FOUND ON THE UPPER HINGES OF DOOR # 2 LH AT STA 693.5 LBL 60- RSC TRACKING
- [SDR FDEA202103130634](https://openairdocs.org/sdr/FDEA202103130634.md): Heat Shield · cracked · Mar 13, 2021 · N773FD · Boeing 757222 · Pneumatic Distribution System
  > L/W I/B L/E PNEMATIC DUCT AFTER REMOVAL AND CLEANING COKED HYDRAULIC FLUID, FOUND HEAT SHIELD TO BE CRACKED REMOVED DAMAGE FROM L/W I/B L/E PNEUMATIC DUCT AN APPLIED REPAIR PLIES TO NOTED AREA IAW B757 51-70-17 PARA 4H AND EA# F-3610-T0360331-P1 PNEUMATIC
- [SDR FDEA202103090607](https://openairdocs.org/sdr/FDEA202103090607.md): Angle · cracked · Mar 9, 2021 · N773FD · Boeing 757222 · Nacelle/Pylon, Main Frame
  > #2 PYLON AFT FAIRING O/B SIDE LOWER CHORD FWD ATTACH ANGLE IS CRACKED REMOVE AND REPLACE ANGLE PER BAC DWG #313N3053 REV E AND B757 SRM 51-40-02-OG
- [SDR FDEA202103040565](https://openairdocs.org/sdr/FDEA202103040565.md): Wire Harness · burned · Mar 4, 2021 · N773FD · Boeing 757222 · Electrical Power System Wiring
  > APU POWER FEEDER WIRE BUNDLE W2800 CHAFED AGAINST A CLAMP BRACKET AFT OF THE STA 1720 BULKHEAD WL 280 RBL30. REPAIR PER EA F-2450-T0360171 P1 ELECTRICAL POWER - AUXILIARY POWER UNIT (APU) POWER FEEDER WIRE - WIRE BUNDLE ROUTING CHANGE, SB 757-24-0089, AD 2
- [SDR FDEA202102260477](https://openairdocs.org/sdr/FDEA202102260477.md): Transmitter · failed · Feb 26, 2021 · N773FD · Boeing 757222 · Trailing Flap Position Indicating System
  > TE FLAP ASYM ON FINAL, RAN QRH DECLARED AN EMERGNCY REMOVED AND REPLACED L/H FLAP POSITION TRANSMITTER REF B757 AMM 27-58-03-4, AND PERFORMED ADJUSTMENT TEST, OPS CHECKS GOOD.
- [SDR FDEA202101220177](https://openairdocs.org/sdr/FDEA202101220177.md): Girt Bar · broken · Jan 22, 2021 · N773FD · Boeing 757222 · Emergency Equipment
  > GIRT BAR PART BROKE OFF LEFT FORWARD ENTRY DOOR. REATTACHED GIRT BAR SLIDE, PER MM 25-66-01-4.
- [SDR FDEA201907161572](https://openairdocs.org/sdr/FDEA201907161572.md): Transmitter · inoperative · Jul 16, 2019 · N773FD · Boeing 757222 · Leading Edge Slat Position Indicating System
  > PDIS 773 27-80 4178 16JUL19 BUF OPEN U LOGPAGES:2977364 AFTER TAKEOFF WHEN CLIMBING OUT FLAPS INDCATORS STOPPED BETWEEN 1 AND THE UP POSITION, WITH FLAP HANDLE IN UP POSITION. NO EICAS INDICATIONS. PUT FLAP HANDLE TO 1 AND LE SLAT DISAGREE EIC
- [SDR FDEA201708312453](https://openairdocs.org/sdr/FDEA201708312453.md): Rope · out of position · Aug 31, 2017 · N773FD · Boeing 757222 · Escape Slide
  > ROPE ATTACHED TO SLIDE BINDING AT L1 DOOR PROPERLY INSTALLED AND STOWED GIRT BAR STATIC LINE
- [SDR FDEA201703220967](https://openairdocs.org/sdr/FDEA201703220967.md): Slide · low pressure · Mar 22, 2017 · N773FD · Boeing 757222 · Escape Slide
  > PRESSURE LOW ON RIGHT CREW ENTRY DOOR. REMOVED FAULTY R1 EVACUATION SLIDE ASSEMBLY. INSTALLED A SERVICEABLE SLIDE ASSEMBLY IAW MM 25-66-01-4. OK FOR SERVICE.
- [SDR FDEA201503060697](https://openairdocs.org/sdr/FDEA201503060697.md): Pan · corroded · Mar 6, 2015 · N773FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT STATION 700 - 720, STRINGER 20L - 22L MIDDLE WASTE SERVICE PAN UPPER DOUBLER PLATE CORRODED. REMOVED PER SRM 51-10-02 REV 113 AND FOUND OUT OF LIMITS IAW SRM 53-00-53 FIG 101 ALLOWABLE DAMAGE 1 REV 114 PART 1 OF EA F-5310-T0315975.
- [SDR FDEA201503020626](https://openairdocs.org/sdr/FDEA201503020626.md): Skin · damaged · Mar 2, 2015 · N773FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > TWO ELONGATED HOLES FOUND ON THE EXTERIOR SKIN AT BS 1360, STRINGER 21 - 22L AFTER DOUBLER REMOVED. REPAIRED IAW EA F-5330-T0315211A PART 1. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA201502230583](https://openairdocs.org/sdr/FDEA201502230583.md): Seat Track · chafed · Feb 23, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 515 - 530, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502230582](https://openairdocs.org/sdr/FDEA201502230582.md): Seat Track · chafed · Feb 23, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 538 - 542, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502230581](https://openairdocs.org/sdr/FDEA201502230581.md): Seat Track · chafed · Feb 23, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 560 - 580, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502230580](https://openairdocs.org/sdr/FDEA201502230580.md): Seat Track · chafed · Feb 23, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 610 - 620, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502230579](https://openairdocs.org/sdr/FDEA201502230579.md): Seat Track · chafed · Feb 23, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 464 - 484, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REFER TO DRC 0025 FOR DETAIL REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502070469](https://openairdocs.org/sdr/FDEA201502070469.md): None · none · Feb 7, 2015 · N773FD · Boeing 757222 · Standard Practices/Structures
  > EXISTING REPAIR WING, LT SIDE THERE IS A REPAIR AT LT INBD MAIN FLAP LE SKIN, MF STATION 267 - 300. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A3 PT 1 ATTACHMENT B, NO HISTORY.
- [SDR FDEA201502070516](https://openairdocs.org/sdr/FDEA201502070516.md): None · none · Feb 7, 2015 · N773FD · Boeing 757222 · Standard Practices/Structures
  > EXISTING REPAIR, FUSELAGE EXTERIOR SKIN. THERE IS A REPAIR AT STATION 1462 - 1480, STRINGER 29L - 29R. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A2 PT 1 ATTACHMENT B, NO HISTORY.
- [SDR FDEA201502070502](https://openairdocs.org/sdr/FDEA201502070502.md): Skin · scratched · Feb 7, 2015 · N773FD · Boeing 757222 · Wing, Plate/Skin
  > RIGHT WING, LOWER SKIN LOWER SURFACE FOUND SCRATCHED AT FSS 567, 3 - 12 INCHES FROM SKIN LE. REPAIRED IAW EA F-5730-T0315336 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502070519](https://openairdocs.org/sdr/FDEA201502070519.md): Skin · unknown · Feb 7, 2015 · N773FD · Boeing 757222 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERNAL SKIN FWD LOWER CORNER HAS EXISTING TRIM OFF. COMPLIED WITH EA F-5230-T0315269 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502070501](https://openairdocs.org/sdr/FDEA201502070501.md): Skin · cracked · Feb 7, 2015 · N773FD · Boeing 757222 · Service Doors
  > CABIN R4 DOOR INNER SKIN LIGHTENING HOLE, 1 INCH TO AFT EDGE & 17 INCHES TO LOWER EDGE, FOUND CRACK AT EDGE. REPAIRED IAW EA F-5210-T0315341 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201502070518](https://openairdocs.org/sdr/FDEA201502070518.md): None · none · Feb 7, 2015 · N773FD · Boeing 757222 · Standard Practices/Structures
  > EXISTING REPAIR DOOR. THERE IS A REPAIR AT AFT CARGO DOOR, 16 INCHES FROM FWD & 14 INCHES FROM LOWER EDGE, STATION 1391 - 1400, STRINGER 24R - 26R. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-70A2 PT1 ATTACHMENT B, HISTORY 23.
- [SDR FDEA201502070468](https://openairdocs.org/sdr/FDEA201502070468.md): Shim · migrated · Feb 7, 2015 · N773FD · Boeing 757222 · Wing Main, Frame Structure
  > LEFT WING, TE CAVITY BETWEEN MLG SUPPORT FITTING & UPPER WING SKIN SHIM MIGRATED AT IRSS 310. REPAIRED IAW EA F-5740-T0313756 PT1. REPAIR IS MAJOR.
- [SDR FDEA201502050444](https://openairdocs.org/sdr/FDEA201502050444.md): Support Beam · chafed · Feb 5, 2015 · N773FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON FAN COWL SUPPORT BEAM OTBD RAIL AT NACELLE STATION 75 LOWER SURFACE FOUND CHAFED. REPAIRED IAW EA F-5450-T0315243 PT 1. RAIL GOUGE BLENDED OUT REPAIR. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201502040438](https://openairdocs.org/sdr/FDEA201502040438.md): Skin · chafed · Feb 4, 2015 · N773FD · Boeing 757222 · Wing, Plate/Skin
  > RIGHT WING, LOWER SKIN LOWER SURFACE FOUND CHAFED AT WS 574, 4 INCHES LONG FROM SKIN TE. COMPLIED WITH EA F-5730-T0314870 PART 1.
- [SDR FDEA201502040425](https://openairdocs.org/sdr/FDEA201502040425.md): Skin · scratched · Feb 4, 2015 · N773FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > SCRATCHES ON THE EXISTING REPAIR DOUBLER AT BS 1355 - 1380, STRINGERS 21 - 24L. REPAIRED IAW EA F-5330-T0315211A PART 1.
- [SDR FDEA201502020410](https://openairdocs.org/sdr/FDEA201502020410.md): Panel · chafed · Feb 2, 2015 · N773FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT WING INBD TE, MAIN FLAP UPPER OTBD PANEL, UPPER SURFACE FOUND CHAFE MARK 19 INCHES LONG FROM PANEL OTBD 8" FROM PANEL LE, ITEM ON RACK. REMOVED, DRIED OUT USING 150 DEG F VACUUM PROCESS. REPAIR PARTS INSTALLED USING 250 DEG F HOT BONDING PROCEDURES IAW
- [SDR FDEA201501300394](https://openairdocs.org/sdr/FDEA201501300394.md): Seat Track · chafed · Jan 30, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 1225 RBL 24.75. SEAT TRACK INBD FLANGE FOUND CHAFED MARK. CHAFE REMOVED IAW SRM 51-10-02 REV 113. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE I FIG 101 REV 113. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52 REPAIR I FIG 201 REV. 114.
- [SDR FDEA201501300393](https://openairdocs.org/sdr/FDEA201501300393.md): Seat Track · chafed · Jan 30, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 1560 - 1580 RBL 24.75, SEAT TRACK CROWN. REMOVED IAW SRM 51-10-02 REV 113. REWORKED AREA, EVALUATED & FOUND MATERIAL LOSS OF 0.025 INCHES EXCEEDS CROWN LIMIT OF 0.020 INCHES IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 113. SEAT TRACK REMOVED BETWEEN
- [SDR FDEA201501290365](https://openairdocs.org/sdr/FDEA201501290365.md): Skin Panel · chafed · Jan 29, 2015 · N773FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT WING INBD TE, MAIN FLAP NOSE SKIN LOWER FWD AREA, FOUND A CHAFE AT MF STA 260. REMOVED IAW SRM 51-10-02 REV 113 & FOUND OUT OF LIMITS IAW SRM 57-53-01 FIG 101 ALLOWABLE DAMAGE 1 REV 113. REPAIR CARRIED OUT IAW SRM 57-53-01 REPAIR 3 REV 114. EXAMINE TH
- [SDR FDEA201501290364](https://openairdocs.org/sdr/FDEA201501290364.md): Skin Panel · chafed · Jan 29, 2015 · N773FD · Boeing 757222 · Trailing Edge Flaps
  > LEFT WING INBD TE MAIN FLAP, OTBD PANEL UPPER SURFACE, FOUND CHAFE MARK 12 INCHES LONG FROM PANEL OTBD EDGE, 8 INCHES FROM PANEL LE. REMOVED, DRIED OUT USING 150 DEG F VACUUM PROCESS. REPAIR PARTS INSTALLED USING 250 DEG F HOT BONDING PROCEDURES IAW SRM 57-
- [SDR FDEA201501270308](https://openairdocs.org/sdr/FDEA201501270308.md): Seat Track · chafed · Jan 27, 2015 · N773FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - STA 815 - 830 LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK CROWN CHAFE MARK REMOVED IAW SRM 51-10- 02 REV 113 REWORKED AREA EVALUATED AND FOUND MATERIAL LOSS OF 0.030", EXCEEDED CROWN LIMIT OF 0.20" IAW SRM 53-00-52 ALLOWABLE DAMAGE I FIG 101 R
- [SDR FDEA201501270309](https://openairdocs.org/sdr/FDEA201501270309.md): Strap · cracked · Jan 27, 2015 · N773FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > BS 365 - 377, LBL 24.75 STABILIZER STRAP FOUND CRACKED. R & R IAW DWG 141N5150 SHT 1 REV D. INSTALLED IAW SRM 51-40-02 REV 114 & EA F-5310-T0314639 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201501240284](https://openairdocs.org/sdr/FDEA201501240284.md): Skin · worn · Jan 24, 2015 · N773FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EMPENNAGE LT SIDE BS 1850 - 1870, THERE IS WEAR CAUSED BY THE LOWER HORIZONTAL STABILIZER TO BODY SEAL AT AFT LOWER PORTION OF THE STABILIZER CUT OUT. WEAR REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL VII REV 113. REPAIRED IAW SRM 53-80-01
- [SDR FDEA201501210244](https://openairdocs.org/sdr/FDEA201501210244.md): Bulkhead · damaged · Jan 21, 2015 · N773FD · Boeing 757222 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 PYLON AFT BULKHEAD AFT LOWER FLANGE, FOUND TWO TOOL DAMAGE & TWO DRILLED HOLES. REPAIRED IAW EA. F-5450-T0314203 PT1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201501200237](https://openairdocs.org/sdr/FDEA201501200237.md): Skin · damaged · Jan 20, 2015 · N773FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN NICKED & SCRATCHED AT BS 520 - 540, STRINGER 23 - 24R. NICKS AND SCRATCHES REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113. REPAIRED IAW EA F-5330-T0314821 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N773FD/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 = 'N773FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N773FD/reports

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