# Service difficulty reports: N788FD

A list on [N788FD](https://openairdocs.org/aircraft/N788FD.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 2 · 60 reports

- [SDR FDEA202608041082](https://openairdocs.org/sdr/FDEA202608041082.md): Battery · failed · Aug 4, 2026 · N788FD · Boeing 757222 · Battery/Charger System
  > BETWEEN 16-18000 FT GOT LT, RT, & CENTER IRS DC FAILED. TRIED STARTING APU TO VERIFY HOT BATTERY BUS STILL WORKING. WHEN APU REACHED SPEED GOT EICAS APU FUEL VALVE & RT FUEL SPAR VALVE. MAIN BATTERY CHARGER MSG ILLUMINATED. BTWN IRU FAILS & EICAS MGS NOTICE
- [SDR FDEA202510242090](https://openairdocs.org/sdr/FDEA202510242090.md): Skin · dented · Oct 24, 2025 · N788FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STAB FRONT SPAR UPPER SURFACE DENT STA 159.248 APPROX FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 159.248 OUT OF LIMITS DIM A= 1.500" Y=0.054" A/Y=27.77 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I, NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4
- [SDR FDEA202510242089](https://openairdocs.org/sdr/FDEA202510242089.md): Skin · dented · Oct 24, 2025 · N788FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STAB FRONT SPAR UPPER SURFACE HAS A DENT (STA 86.600) FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 86.600, OUT OF LIMITS DIM A=1.500", Y=0.069", A/Y=21.73 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4
- [SDR FDEA202510232076](https://openairdocs.org/sdr/FDEA202510232076.md): Skin · corroded · Oct 23, 2025 · N788FD · Boeing 757222 · Fuselage Main, Structure
  > AFT POTABLE WATER SERVICE DOOR PAN POSSIBLE CORROSION STA 1681 TO STA1701 BTW STRINGERS 26R TO STR 29R COMPLIED WITH FEDEX EA F-5330-T0385436 P1 TITLE: FUSELAGE-PLATES AND SKINS-AFT LAV PAN CUT OUT SKIN CORROSION REPAIR. MAJOR REPAIR.
- [SDR FDEA202504250652](https://openairdocs.org/sdr/FDEA202504250652.md): Reservoir · empty · Apr 25, 2025 · N788FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR EMERGENCY POWER ASSIST RESERVOIR GAUGE SHOWS EMPTY. REMOVED AND REPLACE DTHE L1 DOOR EMERGENCY POWER RESERVOIR IN REF TO AMM 52-11-30-4. A/C OK FOR SERVICE.
- [SDR FDEA202312101929](https://openairdocs.org/sdr/FDEA202312101929.md): Frame · cracked · Dec 10, 2023 · N788FD · Boeing 757200 · Fuselage Main, Frame
  > CRACK FOUND AT FRAME 1640 RIGHT HAND SIDE COMPLIED WITH ALL STEPS 1-16 OF E.A. TF-5310-T0377033 P1 AND COMPLETED "FUSELAGE- MAINFRAME-STA 1640 FRAME, SPLICE REPAIR BETWEEN STRINGER I-9F AND S-20R-EO F-5310- E0367020 A CRACK INDICATION REPAIR-PARTIAL FRAME RE
- [SDR FDEA202312051917](https://openairdocs.org/sdr/FDEA202312051917.md): Floorboard · damaged · Dec 5, 2023 · N788FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221BF ON VTMAE TRAVELER #T23/1718651 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051915](https://openairdocs.org/sdr/FDEA202312051915.md): Floorboard · damaged · Dec 5, 2023 · N788FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221MBF ON VTMAE TRAVELER # T23/1718650 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051914](https://openairdocs.org/sdr/FDEA202312051914.md): Floorboard · damaged · Dec 5, 2023 · N788FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 FLOORBOARD 221AF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221AF ON VTMAE TRAVELER # T23/1718653 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051913](https://openairdocs.org/sdr/FDEA202312051913.md): Floorboard · damaged · Dec 5, 2023 · N788FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222AF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222AF ON VTMAE TRAVELER # T23/1718647 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051912](https://openairdocs.org/sdr/FDEA202312051912.md): Floorboard · damaged · Dec 5, 2023 · N788FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 FLOORBOARD 222MAF ON VTMAE TRAVELER # T23/1718633 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051911](https://openairdocs.org/sdr/FDEA202312051911.md): Floorboard · damaged · Dec 5, 2023 · N788FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222BF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222BF ON VTMAE TRAVELER # T23/1718643 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202311051828](https://openairdocs.org/sdr/FDEA202311051828.md): Battery · failed · Nov 5, 2023 · N788FD · Boeing 757200 · Emergency Lighting
  > L/H SLIDE LIGHT DOES NOT TURN ON. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK FOR L/H SLIDE LIGHT, REF. AMM 33-51-07-2. L/H SLIDE LIGHT OPS CHECK NORMAL, REF. SAME. OK TO CONTINUE.
- [SDR FDEA202311031825](https://openairdocs.org/sdr/FDEA202311031825.md): Unknown · unknown · Nov 3, 2023 · N788FD · Boeing 757200 · Fire Detection
  > PDIS 788 26-12 6589 03NOV23 BHM FACT U DESCENDING THROUGH 12000 MSL RECEIVED MAIN CARGO FIRE EICAS MESSAGE AND INDICATIONS. INDICATIONS WENT AWAY WHILE RUNNING QRH. AFTER LANDING RECEIVED EQUIPT OVERHEAT. EMERGENCY DECLARED. ***EMERGENCY DECL
- [SDR FDEA202206031370](https://openairdocs.org/sdr/FDEA202206031370.md): Light · inoperative · Jun 3, 2022 · N788FD · Boeing 757200 · Emergency Equipment
  > RT DOOR SLIDE EMERGENCY LIGHT INOP. FACT 04JUN22 18:56 GJT REF WRI 25-60/5466. REMOVED AND REPLACED R1 DOOR AND SLIDE EMERGENCY LIGHT BATTERY HOLDER ASSY AND
- [SDR FDEA202206031371](https://openairdocs.org/sdr/FDEA202206031371.md): Light · inoperative · Jun 3, 2022 · N788FD · Boeing 757200 · Emergency Lighting
  > RT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP REMOVED AND REPLACED R1 DOOR AND SLIDE EMERGENCY LIGHT BATTERY HOLDER ASSY AND BATTERY CHARGER PER AMM 33-51-07-2. SYSTEM OPS NORM.
- [SDR FDEA202112103081](https://openairdocs.org/sdr/FDEA202112103081.md): None · none · Dec 10, 2021 · N788FD · Boeing 757200 · Fuselage Main, Structure
  > STRINGER SPLICE AT STA 1464, STR29L, REQUIRES REPLACEMENT ACCOMPLISHED FEDEX EA# F-5310-T0365675-P1;FUSELAGE -,MAIN FRAME - STRINGER,STA 1430-1460, S29L,SPLICE REPAIR AND STA1460 - STA1489 STRINGER AND STRINGER SPLICE REPAIR IAW B757-200 SRM 53-00-0
- [SDR FDEA202112103080](https://openairdocs.org/sdr/FDEA202112103080.md): Frame · corroded · Dec 10, 2021 · N788FD · Boeing 757200 · Fuselage Main, Structure
  > AFT CARGO LOWER FRAME CORRODED AT STA 1460 BL0 TO RBL 4.5 ACCOMPLISHED FEDEX EA # F-5310-T0365644-P1, FUSELAGE MAIN FRAME, S28L TO S28R SPLICE REPAIR
- [SDR FDEA202111302954](https://openairdocs.org/sdr/FDEA202111302954.md): Bracket · cracked · Nov 30, 2021 · N788FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > EMPENNAGE INTERIOR ABOVE CENTER SECTIONAPU INLET DUCT LOWER SUPPORT BRACKET CRACKED AT BS1864 REMOVED BRACKET, INSTALLED SERVICEABLE BRACKET IAW B757 SRM 51-40-02-0G
- [SDR FDEA202111292948](https://openairdocs.org/sdr/FDEA202111292948.md): Bracket · cracked · Nov 29, 2021 · N788FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > SUPPORT BRACKET AT STA 1864 FOR APU INLET DUCT,CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 353N1043 REV A AND BOEING DWG # 353N1001 REV F
- [SDR FDEA202111292947](https://openairdocs.org/sdr/FDEA202111292947.md): Fitting · damaged · Nov 29, 2021 · N788FD · Boeing 757200 · Elevator Structure
  > R/H ELEVATOR TIP FITTING HAS ELONGATED HOLES UNDER STATIC WICK BASE REPAIRED PER FEDEX EA #F-5520-T0365567-P1
- [SDR FDEA202111242931](https://openairdocs.org/sdr/FDEA202111242931.md): Panel · delaminated · Nov 24, 2021 · N788FD · Boeing 757200 · Wing, Plate/Skin
  > R/W I/B L/E PANEL 611KT HAS COMPOSITE DAMAGE ON THE INNER SURFACE@ CORNER REPAIRED PER FEDEX EA # F-5730-T0365459-P1
- [SDR FDEA202111232926](https://openairdocs.org/sdr/FDEA202111232926.md): Slat · delaminated · Nov 23, 2021 · N788FD · Boeing 757200 · Wing Structure
  > #6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED SLAT PER B757 AMM 27-81-01-4
- [SDR FDEA202111222918](https://openairdocs.org/sdr/FDEA202111222918.md): Door · unknown · Nov 22, 2021 · N788FD · Boeing 757200 · Service Doors
  > R2 DOOR UPPER HINGE CUT OUT REPAIR HAS INCORRECT AND MISSING FASTENERS INSTALLED IAW B757 SRM 52-10-02-2R REMOVED AND REPLACED FASTENERS FOR R2 DOOR UPPER HINGE CUT OUT REPAIR IAW B757-200 SRM 52- 10-02-2R, FIG 201, REPAIR 1, DETAIL III
- [SDR FDEA202111202910](https://openairdocs.org/sdr/FDEA202111202910.md): None · none · Nov 20, 2021 · N788FD · Boeing 757200 · Leading Edge Slat Control System
  > #7 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED #7 SLAT IAW B757 AMM 27-81-02-4 OPS CHECK GOOD.
- [SDR FDEA202111202909](https://openairdocs.org/sdr/FDEA202111202909.md): None · none · Nov 20, 2021 · N788FD · Boeing 757200 · Leading Edge Slat Control System
  > #8 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED #8 SLAT AND OPS TEST IAWB757 AMM 27-81-02-4
- [SDR FDEA202111202908](https://openairdocs.org/sdr/FDEA202111202908.md): None · none · Nov 20, 2021 · N788FD · Boeing 757200 · Leading Edge Slat Control System
  > #4 SLAT SHOWS SKIN TO CORE DISBONDING REMOVED AND REPLACED #4 SLAT AND OPS TEST PER B757 AMM 27-81-02-4
- [SDR FDEA202111192904](https://openairdocs.org/sdr/FDEA202111192904.md): Frame · gouged · Nov 19, 2021 · N788FD · Boeing 757200 · Fuselage Main, Structure
  > EMPENNAGE INTERIOR BELOW CENTER SECTION BILGE AREA FRAME HAS A GOUGE AT BS 1844 RBL 5 REPAIRED PER B757 SRM 51-70-11-OG
- [SDR FDEA202111182891](https://openairdocs.org/sdr/FDEA202111182891.md): None · corroded · Nov 18, 2021 · N788FD · Boeing 757200 · Elevator Structure
  > R/H ELEVATOR TIP UPPER AND LOWER PLATES ARE CORRODED FABRICATED NEW PLATES PER BOEING DWG # 183N2007 REV A
- [SDR FDEA202111112824](https://openairdocs.org/sdr/FDEA202111112824.md): None · cracked · Nov 11, 2021 · N788FD · Boeing 757200 · Engine Cowling System
  > #1 ENG I/B SIDE CORE COWL SPRING SEAL IS CRACKED APPROX 12"AFT OF THE FWD EDGE REMOVED AND REPLACED PER BOEING DWG # 311N3570 REV Y
- [SDR FDEA202111092802](https://openairdocs.org/sdr/FDEA202111092802.md): None · none · Nov 9, 2021 · N788FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > MAIN CABIN RH SIDE AT THE R4 DOOR ENTRANCE STA 1660 UPPER SURFACE OF THE DOOR SILL WEB IS CORRODED REMOVED DAMAGE FROM UPPER SURFACE OF DOOR SILL WEB, STA 1660 RBL 52, ORIGINAL MATERIAL.071, MAT REMOVED.O07", MATERIAL REMAINING.064", FOUND TO BE WITHIN
- [SDR FDEA202111092801](https://openairdocs.org/sdr/FDEA202111092801.md): Deflector · cracked · Nov 9, 2021 · N788FD · Boeing 757200 · Engine Cowling System
  > #1 ENG I/B CORE COWL LOWER LONGERON FWD EDGE SUBSTRUCTURE IS CRACKED REMOVED AND REPLACED DEFLECTOR PER BAC DWG # 314N3210 REV H AND B757 SRM 51-40-02-0G
- [SDR FDEA202002140341](https://openairdocs.org/sdr/FDEA202002140341.md): Lamp · inoperative · Feb 14, 2020 · N788FD · Boeing 757222 · Emergency Lighting
  > L1 DOOR EXTERIOR EMER EXIT LIGHT INOP RELAMPED L1 DOOR EXT EMER EXIT LIGHT (SLIDE LIGHT) USING LAMP P/N 767 LIGHT CHECKS GOOD. REF B757 AMM 33-51-06-2-1. OK FOR SERVICE
- [SDR FDEA2019122083258](https://openairdocs.org/sdr/FDEA2019122083258.md): Strap · dented · Dec 18, 2019 · N788FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > MAIN EQUIPMENT CENTER CEILING AREA,, MAIN FLOOR STRUCTURE ATTACH STABILIZER STRAP HAS A CRACK AT FASTENER HOLE ABOUT 1.5" LONG, BS.480 RBL. 24.75 CUT DAMAGED AT STABILIZER STRAP IAW B757 SRM 51-10-02-0G AND SRM 53-00-51-2R FIG 201 DETAILV REP 12, FAB
- [SDR FDEA201912133241](https://openairdocs.org/sdr/FDEA201912133241.md): Stringer Splice · corroded · Dec 13, 2019 · N788FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE SKIN BULGE AT BS 1464 STR29L APPROX. SUSPECT OF CORROSION EVALUATED AREA AT LWR FUSE SKIN FOUND STR SPLICE CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW STRINGER SPLICE AS PER SRM 51-40-02-0G, 51-10-02-0G AND DWG 146N3820 REV C
- [SDR FDEA2019121323230](https://openairdocs.org/sdr/FDEA2019121323230.md): Angle · corroded · Dec 12, 2019 · N788FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF APU INTAKE DUCT FOUND ANGLE CORRODED APPROX STA 1787 TO 1800 RBL6. FOUND ANGLE AT APU INTAKE DUCT TO BE 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-15. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 148N3152 REV -.
- [SDR FDEA2019100312380](https://openairdocs.org/sdr/FDEA2019100312380.md): Solenoid Valve · leaking · Oct 1, 2019 · N788FD · Boeing 757222 · Hydraulic System, Main
  > RIGHT HYD QTY EICAS MESSAGE INFLIGHT. COMPLIED WITH QRH. FOUND LEAK AT RT SYSTEM APCS ELECTROHYDRAULIC SOLENOID VALVE WHERE IT MATES TO THE SOLENOID. REMOVED AND REPLACED METAL GASKET ON SOLENOID VALVE IAW MM 22-12-02-2. PERFORMED OPS AND LEAK CHECKS. OPS
- [SDR FDEA2018122103564](https://openairdocs.org/sdr/FDEA2018122103564.md): Liner · out of adjust · Dec 20, 2018 · N788FD · Boeing 757222 · Service Doors
  > PDIS 788 25-60 2763 20DEC18 MEM FACT U LOGPAGES:2992755 R FWD DOOR ARMED PANEL DOSN'T EXTEND FACT 20DEC18 06:30 MEM U ADJUSTED R-1 DOOR LINING- DOOR ARMED PANEL(KNUCKLE KNOCKER) OPS CHKS GOOD- REF: B757 M/M 52-11-02-4
- [SDR FDEA201804231094](https://openairdocs.org/sdr/FDEA201804231094.md): Socket · shorted · Apr 23, 2018 · N788FD · Boeing 757222 · Light System Wiring
  > RIGHT EXTERIOR EMERGENCY LIGHT FOR R1 DOOR INOPERATIVE. REMOVED LIGHT SOCKET AND REFLECTOR FROM OUTSIDE OF AIRCRAFT AS PER SB 33-0012 IAW AMM 33-51-06-2-1. TROUBLESHOT IAW WDM 33-51-12, PG 902. FOUND GOOD POWER AND GROUND AT LIGHT ASSY L30. FOUND THAT T
- [SDR FDEA201707151969](https://openairdocs.org/sdr/FDEA201707151969.md): Power Supply · bent · Jul 15, 2017 · N788FD · Boeing 757222 · Emergency Lighting
  > RIGHT EXTERNAL EMERGENCY SLIDE LIGHT FAILED AN OPS TEST. REPLACED THE POWER SUPPLY IAW MM 33-51-07-2, OPS CHECKED OK.
- [SDR FDEA201602260691](https://openairdocs.org/sdr/FDEA201602260691.md): Torque Tube · loose · Feb 26, 2016 · N788FD · Boeing 757222 · Trailing Edge Flap Control System
  > AFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 1 TO FLAPS 0, HAD EICAS MESSAGE, LE FLAP ASYM, & AMBER LIGHT LE. RETURNED TO LAND IAW QRH FAULT CODE FRM 27 90 24 00. INSTALLED TORQUE TUBE COUPLER AND OPS CHECKED LEADING EDGE SLAT SYSTEM IN REF 27-81-00-5 AN
- [SDR FDEA201512073929](https://openairdocs.org/sdr/FDEA201512073929.md): Skin · chafed · Dec 7, 2015 · N788FD · Boeing 757222 · Wing, Plate/Skin
  > PANEL 655AR EXTERNAL SKIN HAS CHAFED. REPAIRED IAW EA F5750-T0320958. MAJOR REPAIR.
- [SDR FDEA201511253777](https://openairdocs.org/sdr/FDEA201511253777.md): Skin · dented · Nov 25, 2015 · N788FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
  > REWORK OF NR N00207, VERTICAL STAB LT SIDE AUXILIARY PANEL HAS DENT, 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM, DUE TO PER NOTED SRM. A VISUAL & NDT INSPECTION OF DAMAGED AREA FOR DISBONDS, DELAMINATION, IS REQUIRED PRIOR TO APPLYING REPAIR. THIS WAS NOT DOC
- [SDR FDEA201511233763](https://openairdocs.org/sdr/FDEA201511233763.md): Flap · cracked · Nov 23, 2015 · N788FD · Boeing 757222 · Trailing Edge Flaps
  > DURING SURVEILLANCE CHECK, A CRACK WAS NOTED, APPROX 1/2", ON LT WING INBD MAIN FLAP, MID TE. REPAIRED CRACK ON LT WING INBD MAIN FLAP, MID TE, LOCATED AT TE, 111.5" OTBD OF MF STATION 74.0. PN 113N2003-47H, SN 000539, FINAL REPAIR 7.5" X 3.25". COMPLIED WI
- [SDR FDEA201511173669](https://openairdocs.org/sdr/FDEA201511173669.md): Skin Panel · delaminated · Nov 17, 2015 · N788FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB RT SIDE, AUXILIARY PANEL HAS DELAMINATION, 26" FROM AUXILIARY SPAR & 120" FROM BOTTOM. REMOVED DAMAGED PANEL ASSEMBLY & INSTALLED NEW PANEL ASSEMBLY PN 175N2001-4, IAW SRM 51-40-02 & WG 175N2001, SHEET 1 AT RT SIDE VERTICAL STAB. MAJOR REPAIR.
- [SDR FDEA201511103547](https://openairdocs.org/sdr/FDEA201511103547.md): Skin · corroded · Nov 10, 2015 · N788FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
  > AFTER PREPARING THE REPAIR AREA ON THE VERTICAL STAB AUXILIARY PANEL DENT, FOUND A DISBONDED AREA OF APPROX 13" X 13" DUE TO CORROSION ON THE INNER SKIN. THIS DISBONDED AREA IS APPROX 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM. REPAIRED LT VERTICAL STAB AUXIL
- [SDR FDEA201510193278](https://openairdocs.org/sdr/FDEA201510193278.md): Skin · dented · Oct 19, 2015 · N788FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAS DENT WITH ASSOCIATED SCRATCH, BELOW STRINGER 24R & FWD OF BS 1768. NOTED DURING EVALUATION OF NR N00049, ACCOMPLISHED EA F-5330-T0320261. FUSELAGE SKIN CREASE, GOUGE & DEEP SCRATCH DAMAGES, BETWEEN BS 1763 & BS 1773, STRINGER 24R T
- [SDR FDEA201510133188](https://openairdocs.org/sdr/FDEA201510133188.md): Skin · dented · Oct 13, 2015 · N788FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT SKIN DENT BETWEEN STATION 1380 - 1400, JUST BELOW AFT CARGO DOOR CUT OUT. ACCOMPLISHED EA F-5330-T0320147. FUSELAGE SKIN REPAIR BETWEEN BS 1380 - 1400 & NR 2 CARGO DOORWAY LOWER MAIN SILL & STRINGER 29R. THIS IS A CAT B REPAIR, MAJOR REPAIR.
- [SDR FDEA201510093154](https://openairdocs.org/sdr/FDEA201510093154.md): Skin · corroded · Oct 9, 2015 · N788FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > PITTING CORROSION RUNNING UP UNDER LAP SEAM AT STRINGER 19L, BS 753 - 780. ACCOMPLISHED EA F-5330-T0320609. CATEGORY B REPAIR, MAJOR REPAIR.
- [SDR FDEA201510073109](https://openairdocs.org/sdr/FDEA201510073109.md): Skin · punctured · Oct 7, 2015 · N788FD · Boeing 757222 · Trailing Edge Flaps
  > LEFT WING INBD FLAP EXTERNAL UPPER SKIN HAS PUNCTURE AT 3 LOCATIONS. REPAIRED LT WING AT 3 LOCATIONS IAW SRM 51-70-06-0G. REF EA F-5750-T0320431 ISSUED FOR TRACKING. CATEGORY A REPAIR MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N788FD/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 = 'N788FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N788FD/reports

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