# Service difficulty reports: N782FD

A list on [N782FD](https://openairdocs.org/aircraft/N782FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA202204190992](https://openairdocs.org/sdr/FDEA202204190992.md): Floorboard · damaged · Apr 19, 2022 · N782FD · Boeing 757200 · Fuselage Floor Panel
  > MDIS 782 53-21 5101 23MAR22 ORF FACT U RAMP REPORTED A HOLE IN AFT CARGO COMP FLOOR @STA 1500. HOLE @ 1" OIL 23MAR22 16:19 ORF U NO RESTRICTION REF: SR57-53-001 ONE HOLE IN AFT CARGO FLOOR AT STA 1500 1" IN DIA. TEMP REPAIR INSTALLED
- [SDR FDEA202107291889](https://openairdocs.org/sdr/FDEA202107291889.md): Slide · detached · Jul 29, 2021 · N782FD · Boeing 757222 · Escape Slide
  > WITH THE R2 DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRD BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R&R R1 DOOR SLIDE IAW B757 AMM 25-66-01-4.
- [SDR FDEA202107271871](https://openairdocs.org/sdr/FDEA202107271871.md): Slide · detached · Jul 27, 2021 · N782FD · Boeing 757222 · Escape Slide
  > WITH THE R2 (UPDATED TO REFLECT R1) DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRT BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R & R DOOR ESCAPE SLIDE IAW AMM 25-66-01-4, ASSI
- [SDR FDEA202102230436](https://openairdocs.org/sdr/FDEA202102230436.md): Adc · failed · Feb 23, 2021 · N782FD · Boeing 757222 · Air Data Computer
  > PDIS 782 34-11 4300 23FEB21 MDT FACT U LOG PAGES: 2980148 FO AIR DATA INSTRUMENTS WENT BLANK DURING TO ROLL. R/I 23FEB21 05:38 MDT U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 4040800-912 POS: 2 SRL: 90032121 TAG NBR: 6852G2 ON MPN: 4040800-912 C
- [SDR FDEA202101140097](https://openairdocs.org/sdr/FDEA202101140097.md): Spring · broken · Jan 14, 2021 · N782FD · Boeing 757222 · Main Landing Gear
  > LT GEAR SPRING RETAINER ASSEMBLY BROKEN AT THE START OF LT GEAR OPERATION CHECK. SDR ENTERED IN ERROR AGAINST WRONG TAIL NUMBER.
- [SDR FDEA2020080711743](https://openairdocs.org/sdr/FDEA2020080711743.md): Intercostal · damaged · Aug 1, 2020 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > FUSELAGE SKIN BULGED FROM BS 1420 TO 1440, AT INTERCOSTAL BETWEEN STRINGERS 28R AND 29R. REMOVED, FABRICATED, AND INSTALLED THE NEW INTERCOSTAL IAW DWG 146N5398, REV P, A, DWG 146N5425 REV -, AND SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN
- [SDR FDEA2020080511743](https://openairdocs.org/sdr/FDEA2020080511743.md): Intercostal · unknown · Aug 1, 2020 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > FUSELAGE SKIN BULGE FROM BS1420 TO BS1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P, A, SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE INTERCO
- [SDR FDEA2020080311743](https://openairdocs.org/sdr/FDEA2020080311743.md): Intercostal · damaged · Aug 1, 2020 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > FUSELAGE SKIN BULGE FROM BS 1420 TO BS 1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P, A, B757 SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE
- [SDR FDEA201909052122](https://openairdocs.org/sdr/FDEA201909052122.md): Floor Panel · punctured · Sep 5, 2019 · N782FD · Boeing 757222 · Fuselage Floor Panel
  > RAMP REPORTED SMALL PUNCTURE IN FLOOR OF AFT CARGO COMPARTMENT. HOLE IS LOCATED AT APPROX STA 1372 RT SIDE APPROX 8 INCHES FWD OF LOWER AFT CARGO DOOR OPENING. COMPLIED WITH EA F-5321-T0349330 PT1. PATCH III INSTALLED OVER PUNCTURE.
- [SDR FDEA2019061321274](https://openairdocs.org/sdr/FDEA2019061321274.md): Circuit Card · failed · Jun 12, 2019 · N782FD · Boeing 757222 · Landing Gear Position and Warning
  > INTERMITTENT GEAR NOT DOWN WARNING FOR DURATION OF FLIGHT UNTIL GEAR EXTENDED SHGN 11JUN19 16:26 MEM U PERFORMED BITE PROCEDURE FOR PSEU PER 757 FIM 32_09 F/T_802 NO FAULTS STORED. PERFORMED PSEU GROUND TEST FOR SYS #1 AND SYS #2 LDG GEAR SYSTEMS; BOT
- [SDR FDEA201807101658](https://openairdocs.org/sdr/FDEA201807101658.md): Skin · dented · Jul 10, 2018 · N782FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > DENT ON OUTER FUSELAGE SKIN BETWEEN STA 420 & STA 440 BETWEEN S-17L & S-18L. MEASURED, CUT OUT AND REPAIRED DENTED AREA ON FUSELAGE SKIN IAW SRM 5-40-02-0G, SRM 51-40-05-0G AND SRM 53-00-00-01-2R REPAIR 16.
- [SDR FDEA201607072300](https://openairdocs.org/sdr/FDEA201607072300.md): Frame · corroded · Jul 7, 2016 · N782FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO BAY, BS 1400 STRINGERS 29R - 29L FRAME WEB CORRODED, BOTH FRONT AND AFT SURFACE. FRAME REMOVED AND REPLACED IAW DWG 146N1011 SHT 3 REV E. FRAME FABRICATED IAW DWG 146N1028 SHT 8 REV D. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201607012208](https://openairdocs.org/sdr/FDEA201607012208.md): Web · corroded · Jul 1, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY, BS 1460-1480 CARGO DOOR LOWER SILL WEB CORROSION. SILL WEB R&R WITH NEW FABRICATED STA 1460-1480 CARGO DOOR SILL LOWER SILL WEB IAW DWG 146N8522, SHT 7, REV C. NEW LOWER SILL WEB FABRICATED IAW DWG 146N8522-42, SHT 7, REV C. REPAIR CLASSIFIED
- [SDR FDEA201606282158](https://openairdocs.org/sdr/FDEA201606282158.md): Dome Nut · corroded · Jun 28, 2016 · N782FD · Boeing 757200 · Passenger/Crew Doors
  > CABIN L1 DOOR INTERNAL UPPER WEB, 03 EA DOME NUTS FOUND CORRODED.
- [SDR FDEA201606272154](https://openairdocs.org/sdr/FDEA201606272154.md): Skin · chafed · Jun 27, 2016 · N782FD · Boeing 757222 · Wing, Plate/Skin
  > RT WING, UPPER INTERSPAR SKIN, UPPER SURFACE FOUND CHAFE MARK AT WBL 76-78, 20" LONG FROM SKIN T/E, WING TO BODY FAIRING MATING AREA. MINOR CHAFE MARK BLEND OUT ON 112N3101-12, AFT MACHINED SKIN AT APPROX WBL 76.00 TO 78.00. TRACE FROM REAR SPAR TO STRINGER
- [SDR FDEA201606242134](https://openairdocs.org/sdr/FDEA201606242134.md): Frame · corroded · Jun 24, 2016 · N782FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, STA 1480, STR 27R-26R, FRAME WEB CORROSION FOUND AFTER ATTACHED ANGLE REMOVED.
- [SDR FDEA201606212075](https://openairdocs.org/sdr/FDEA201606212075.md): Stringer Splice · corroded · Jun 21, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY BS 1460 STRINGER 30 STRINGER SPLICE HAS CORROSION. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW DWG 146N3400 SHT 2 REV C. STRINGER SPLICE FABRICATED IAW DWG 146N3820 SHT 01 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201606141997](https://openairdocs.org/sdr/FDEA201606141997.md): Frame · gouged · Jun 14, 2016 · N782FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, BS 1520, STR 22R-STR 23R. FRAME WEB HAS GOUGE MARKS.
- [SDR FDEA201606131972](https://openairdocs.org/sdr/FDEA201606131972.md): Stringer · corroded · Jun 13, 2016 · N782FD · Boeing 757200 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, STA 1618, STR 21L, STRINGER HAS CORROSION. STRINGER REMOVED AND REPAIR IAW SRM 51-40-02 AND SRM 53-00-03, REPAIR 2, REV 118. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201606091905](https://openairdocs.org/sdr/FDEA201606091905.md): Frame · corroded · Jun 9, 2016 · N782FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, BS 1460, STR 26R-28L, FRAME WEB CORROSION. R & R WITH NEW FABRICATED FRAME WEB IAW DWG 146N1014, SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201606091896](https://openairdocs.org/sdr/FDEA201606091896.md): Skin · damaged · Jun 9, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE RT SIDE, THERE IS A LIGHTNING STRIKE AT BS 680 - BS 700 BETWEEN STR 24- STR 25. LIGHTNING STRIKE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 101, DETAIL II, REV 118. REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 118. THIS IS A
- [SDR FDEA201606071858](https://openairdocs.org/sdr/FDEA201606071858.md): Stringer · corroded · Jun 7, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STATION 1510 - 1530, STRINGER 29R, STRINGER CORROSION. CORROSION OUT OF LIMITS, R & R WITH NEW STR STA 1460-STA 1620, STR 29R IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F IN REF TO JOB CARD N02233 IAW WORK DETAIL ATTACHED.
- [SDR FDEA201606071857](https://openairdocs.org/sdr/FDEA201606071857.md): Stringer · corroded · Jun 7, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STATION 1460 - 1480, STRINGER 29R, STRINGER CORROSION. AFT CARGO COMPARTMENT OUT OF LIMIT, STR STA 1460-STA 1620, STR 29R. R & R WITH NEW STR STA 1460-STA 1620 IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F. REPAIR CLASSIFI
- [SDR FDEA201606061855](https://openairdocs.org/sdr/FDEA201606061855.md): Skin · damaged · Jun 6, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE RIGHT SIDE THERE IS A LIGHTNING STRIKE AT BS 500 - 520 BETWEEN STRINGER 25 - 26 WITH STICKER 633. LIGHTNING STRIKE MARK REMOVED AREA FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX, AD REPAIR CARRIED OU
- [SDR FDEA201606061854](https://openairdocs.org/sdr/FDEA201606061854.md): Skin · damaged · Jun 6, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 480 - 500, BETWEEN STRINGER 25 - 26 WITH STICKER 630. FUSELAGE EXTERIOR SKIN AT BS 480-500, STR 25R-26R LIGHTING STRIKE MARK. REMOVED AREA, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPT
- [SDR FDEA201606061853](https://openairdocs.org/sdr/FDEA201606061853.md): Skin · damaged · Jun 6, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 460 - 480, BETWEEN STRINGER 25 - 26 WITH STICKER 613. REMOVED AREA, FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX AND REPAIR CARRIED OUT IAW SRM 53-00-01, FI
- [SDR FDEA201606051849](https://openairdocs.org/sdr/FDEA201606051849.md): Frame · corroded · Jun 5, 2016 · N782FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT STATION 1560, STRINGER 30 - 29L, FRAME WEB CORROSION.
- [SDR FDEA201606051848](https://openairdocs.org/sdr/FDEA201606051848.md): Skin · chafed · Jun 5, 2016 · N782FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT WING OTBD TE MAIN FLAP, NOSE SKIN FOUND CHAFE MARK AT 2.5" FROM OTBD EDGE.
- [SDR FDEA201605311764](https://openairdocs.org/sdr/FDEA201605311764.md): Channel · damaged · May 31, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD CHANNEL, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CHANNEL REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD CHANNEL FABRICATED IAW DWG 146N5317, SHT 1, REV AND INSTALLED IAW DWG 146N5300, SHT 23
- [SDR FDEA201605311763](https://openairdocs.org/sdr/FDEA201605311763.md): Angle · damaged · May 31, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD ANGLE, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CABIN, STA 1720, LBL 65-RBL 65 DECK PLATE ATTACHED CHORD ANGLE WITH ELONGATED HOLE REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD ANGLE INSTALL
- [SDR FDEA201605261739](https://openairdocs.org/sdr/FDEA201605261739.md): Stringer Splice · corroded · May 26, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, STATION 1460, STRINGER 28L, STRINGER SPLICE HAS CORROSION. R & R WITH NEW FABRICATED STA 1460, STR 28L, STRINGER SPLICE IAW DWG 146N3400, SHT 02, REV C. NEW STRINGER FABRICATED IAW DWG 146N3820, SHT 01, REV C.
- [SDR FDEA201605261738](https://openairdocs.org/sdr/FDEA201605261738.md): Frame Splice · gouged · May 26, 2016 · N782FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, STATION 1520, STRINGER 24R, FRAME SPLICE HAS GOUGE MARKS. FRAME SPLICE REMOVED AND REWORKED AREA TREATED IAW SRM 51-10-02 AND SRM 51-20-01, REV 118. MATERIAL REMOVED 0.027" OUT OF LIMIT. FRAME SPLICE R & R WITH NEW FABRICATED FRAME SP
- [SDR FDEA201605141582](https://openairdocs.org/sdr/FDEA201605141582.md): Floorbeam · corroded · May 14, 2016 · N782FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN STATION 1681, RBL 10 - 47, FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVAL. CABIN, STA 1681, RBL 10-47 FLOORBEAM UPPER FLANGE CORROSION REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA ORIGINAL THICKNESS 0.158" MATERIAL THICKNESS. REMA
- [SDR FDEA201605091517](https://openairdocs.org/sdr/FDEA201605091517.md): Strap · corroded · May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer Structure
  > RIGHT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRCIATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201605091515](https://openairdocs.org/sdr/FDEA201605091515.md): Strap · corroded · May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer Structure
  > LEFT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRICATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201605091516](https://openairdocs.org/sdr/FDEA201605091516.md): Strap · corroded · May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer Miscellaneous Structure
  > EMPENNAGE, RT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP. FOUND CORROSION RT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP REMOVED AND NEW PIVOT FABRICATED IAW DWG NR: 182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601, SHT 1, REV C.
- [SDR FDEA201605091514](https://openairdocs.org/sdr/FDEA201605091514.md): Strap · corroded · May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer Miscellaneous Structure
  > EMPANNAGE, LEFT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP FOUND CORROSION LT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP. REMOVED AND NEW PIVOT STRAP FABRICATED IAW DWG NR:182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601 SHT, REV
- [SDR FDEA201605071494](https://openairdocs.org/sdr/FDEA201605071494.md): Intercostal · corroded · May 7, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CABIN STATION 1621, STRINGER 13L INTERCOSTAL WEB FOUND CORROSION. INTERCOSTAL WEB CORROSION REMOVED IAW SRM 51-12-02 REV 117. FOUND 50% MATERIAL LOSS. INTERCOSTAL WEB R & R WITH FABRICATED WEB IAW SRM 51-40-02 REV 117 & DWG 146N8734 SHT 1 REV C. INTERCOST
- [SDR FDEA201605041457](https://openairdocs.org/sdr/FDEA201605041457.md): Deck Plate · corroded · May 4, 2016 · N782FD · Boeing 757222 · Fuselage Floor Panel
  > BS 1681 LBL 10 - 17 DECK PLATE UPPER SURFACE FOUND CORRODED. COMPLIED WITH EA F-5310-T0325421 PART 1 P1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201605041453](https://openairdocs.org/sdr/FDEA201605041453.md): Pan · chafed · May 4, 2016 · N782FD · Boeing 757222 · Passenger/Crew Doors
  > CABIN L1 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 117. FOUND EXCEEDS LIMIT IAW SRM 52-10-01-1A REV 117. HANDLE PAN REMOVED IAW SRM 51-40-02 REV 117 & REPLACED IAW DWG 141N6100 SHT 8 REV K & SHT 14 REV F. REPAIR CLASSIFIED MAJOR I
- [SDR FDEA201605031445](https://openairdocs.org/sdr/FDEA201605031445.md): Seat Track · chafed · May 3, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 1550 - 1570, LBL 24.75 SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEAN UP DEPTH ON THE LIP OF SEAT TRACK CROWN 0.040" AFTER REMOVAL THE MAXIMUM DIAMETER BETWEEN THE LIPS 0.504" EXCEED THE MAXIMUM LIMIT 0.48
- [SDR FDEA201604281420](https://openairdocs.org/sdr/FDEA201604281420.md): Floorbeam · damaged · Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN STATION 1440, RBL 19, FLOORBEAM UPPER FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-51-2R FIG 201 REPAIR 5 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM.
- [SDR FDEA201604281419](https://openairdocs.org/sdr/FDEA201604281419.md): Seat Track · damaged · Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 1316, RBL 45.5, SEAT TRACK OTBD FLANGE HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 OPTION 1 REV 117. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201604281418](https://openairdocs.org/sdr/FDEA201604281418.md): Seat Track · damaged · Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 1475, LBL 24.75, SEAT TRACK INBD FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 REPAIR 1 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201604281417](https://openairdocs.org/sdr/FDEA201604281417.md): Seat Track · chafed · Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 1590, RBL 45.5 SEAT TRACK INBD FLANGE CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEANED UP DEPTH OF 0.021" MATERIAL ORIGINAL, THICKNESS 0.080" AND REMAINING THICKNESS 0.059" FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-00-52-1A
- [SDR FDEA201604221350](https://openairdocs.org/sdr/FDEA201604221350.md): Crease Beam · corroded · Apr 22, 2016 · N782FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN 1360 - 1380 RT CREASE BEAM WEB UPPER SURFACE FOUND CORROSION. CORROSION, REMOVED IAW SRM 51-10-02, REV 117. MATERIAL REMOVED 0.010" FOUND EXCEED LIMIT IAW SRM 53-60-13-1A, REV 117. CORRODED CREASEBEAM WEB. R & R IAW SRM 51-40-02, REV 117 & DWG 146N55
- [SDR FDEA201604221338](https://openairdocs.org/sdr/FDEA201604221338.md): Crease Beam · corroded · Apr 22, 2016 · N782FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 940 - 960 RT CREASE BEAM WEB FOUND CORROSION. R & R IAW SRM 51-40-02 REV 117 & DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201604141213](https://openairdocs.org/sdr/FDEA201604141213.md): Support · cracked · Apr 14, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CABIN STATION 680 - 698, RBL 24.75, SEAT TRACK SUPPORT FOUND CRACK & CORROSION. COMPLIED WITH EA F-5310-T0325422A PART: 1, P1 TITLE: FUSELAGE, MAINFRAME SEAT TRACK SUPPORT INSTALLATION, BETWEEN STA 640 AND STA 700, RBL 24.75. REPAIR CLASSIFIED AS MAJOR.

## 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 = 'N782FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N782FD/reports

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