# Service difficulty reports: N798FD

A list on [N798FD](https://openairdocs.org/aircraft/N798FD.md).

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

- [SDR FDEA202210132564](https://openairdocs.org/sdr/FDEA202210132564.md): Flap · gouged · Oct 13, 2022 · N798FD · Boeing 757 · Wing, Plate/Skin
  > RT WING I/B MAIN FLAP O/B SIDE TOP SKIN HAS GOUGE MARK. REPAIRED RT WING I/B MAIN FLAP O/B SIDE TOP SKIN IAW SRM 51-70-10 REPAIR #4 PARA 8 TO 9 AND SRM 57-53-01-1A FIG 101 DETAIL VI, MAJOR REPAIR
- [SDR FDEA202210022453](https://openairdocs.org/sdr/FDEA202210022453.md): Floorboard · delaminated · Oct 2, 2022 · N798FD · Boeing 757222 · Fuselage Floor Panel
  > COURIER AREA FLOOR BOARD 221MBF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VTMAE TRAVELER T22/1637405 IAW DWG. SRZ- 25-005 REV. R MAJOR REPAIR.
- [SDR FDEA202208312120](https://openairdocs.org/sdr/FDEA202208312120.md): Gust Lock · cracked · Aug 31, 2022 · N798FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK BROKEN. REMOVED GUST LOCK. OK TO CONTINUE. DOOR OPEN AND CLOSES NORMALLY. REMOVED BROKEN L1 DOOR GUST LOCK COLLAR AND INSTALLED NEW SPLIT COLLAR AND CATCH IAW B757 AMM 52-11-08-8. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. A/C OK FOR SERVI
- [SDR FDEA202012163170](https://openairdocs.org/sdr/FDEA202012163170.md): Pump · failed · Dec 16, 2020 · N798FD · Boeing 757222 · Hydraulic Pump (Electric/Engine), Main
  > AT BLOCK IN HAD LARGE HYDRAULIC LEAK IN LEFT MLG WHEEL WELL. SHIFT NOTE: A/C 798 GROUND EMERGENCY AT BLOCK-IN MX SUSPECTED FIRE IN LEFT WHEEL WELL. FOUND LEFT HYDRAULIC ACMP FAILED. LEFT SYSTEM WAS LEAKING OUT OF ACMP. REMOVED LEFT ACMP, PER AMM 29-11-01-
- [SDR FDEA202010192557](https://openairdocs.org/sdr/FDEA202010192557.md): Paint · deteriorated · Oct 19, 2020 · N798FD · Boeing 757222 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON AFT FIXED INBOARD SIDE ABOVE EXHAUST NOZZLE HAS PAINT DETERIORATED AND EVIDENCE OF CORROSION. REPAIRED AFT FAIRING SKIN, IAW B757-200 SRM 54-51-70-01 AND 54-51-70-2R REPAIR 4.
- [SDR FDEA202010192558](https://openairdocs.org/sdr/FDEA202010192558.md): Structure · damaged · Oct 19, 2020 · N798FD · Boeing 757222 · Fuselage Main, Structure
  > CUSTOMER REQUEST, EVALUATE FASTENER SPACING ON ATTACHMENT ANGLE AT BL 0 FWD OF FRAME AT STA 231.25. REMOVED AND REPLACED CHORD AND INTERCOSTAL, PER DWG 141N8222 AND EA F-5310-T0357422. TITLE;FUSELAGE-MAINFRAME-INTERCOSTAL, STA 273 TO 231, BL 0.
- [SDR FDEA202010162532](https://openairdocs.org/sdr/FDEA202010162532.md): Skin · dented · Oct 16, 2020 · N798FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
  > RT RUDDER SKIN HAS A DENT BETWEEN RUDDER STA 231.852 AND 306.371 AND APPROXIMATELY 33" INCHES FROM THE TRAILING EDGE. MARKED REPAIRED DENT ON RT RUDDER SKIN, IAW B757 SRM 55-40-01-2R AND 51-70-03 PARA 5 L.
- [SDR FDEA202010162530](https://openairdocs.org/sdr/FDEA202010162530.md): Structure · delaminated · Oct 16, 2020 · N798FD · Boeing 757222 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE INBOARD FAN COWL HAS LARGE AREA OF EXPOSED COMPOSITE MATERIAL. REMOVED AND REPLACED INBOARD FAN COWL, IAW B757 AMM 7-1-11-04-4.
- [SDR FDEA202010152515](https://openairdocs.org/sdr/FDEA202010152515.md): Frame · cracked · Oct 15, 2020 · N798FD · Boeing 757222 · Fuselage Main, Frame
  > HOLE AT STA 1640LH BELOW STR 14L HAS CRACK INDICATION. ACCOMPLISHED EA F-5310-T0357159: FUSELAGE-MAINFRAME-FRAME STA 1640 S-14L CRACK INDICATION. THIS EA DEVIATES FROM EO F-5310-E0344602.
- [SDR FDEA202010152514](https://openairdocs.org/sdr/FDEA202010152514.md): Strap · corroded · Oct 15, 2020 · N798FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > NUTPLATE STRAP CORRODED AT STA 1721 LEFT SIDE ABOVE PNEUMATIC DUCT. REMOVED AND REPLACED NUTPLATE STRAPS, IAW B757 SRM 51-40-02 B757 SRM 51-20-01, BOEING DWG: 146N5693 REV: B. ACCOMPLISHED EA: F-5321-T0357460-P1 FUSELAGE-CARGO COMP FLOORS -FLOOR SUPPORT, ST
- [SDR FDEA202010132483](https://openairdocs.org/sdr/FDEA202010132483.md): Nut Plate · corroded · Oct 13, 2020 · N798FD · Boeing 757222 · Fuselage Main, Attach Fittings
  > NUTPLATE STRAP AND NUTPLATE ARE CORRODED ON FLOORBEAM BS 1681.8 LBL 24. REMOVED CORROSION, IAW B757 SRM 53-00-51-1A AND REPLACED NUTPLATE STRAP, IAW BOEING DWG 146N5693 REV B.
- [SDR FDEA202010132482](https://openairdocs.org/sdr/FDEA202010132482.md): Nut Plate · corroded · Oct 13, 2020 · N798FD · Boeing 757222 · Fuselage Main, Attach Fittings
  > NUTPLATE STRAP AND NUTPLATE ARE CORRODED 2 PLACES LEFT SIDE ABOVE PNEUMATIC DUCT BS 1681.8. REMOVED CORROSION, IAW B757 SRM 53-00-51-1A. REPLACED NUTPLATE STRAP, IAW DWG 146N5693 REV B.
- [SDR FDEA202010122463](https://openairdocs.org/sdr/FDEA202010122463.md): Panel · cracked · Oct 12, 2020 · N798FD · Boeing 757222 · Trailing Edge Flaps
  > PARTS RACK, LT WING FLAP FAIRING PANEL 574ER IS CRACKED. RECEIVED NEW PANEL (574ER) P/N 113N1712U4, PER B757 IPC 27-51-31-03.
- [SDR FDEA202010082442](https://openairdocs.org/sdr/FDEA202010082442.md): Bottle · defective · Oct 8, 2020 · N798FD · Boeing 757222 · Emergency Equipment
  > R1 DOOR POWER ASSIST HAS LOW PRESSURE. REMOVED DEFECTIVE BOTTLE AND INSTALLED NEW PART.
- [SDR FDEA202008181925](https://openairdocs.org/sdr/FDEA202008181925.md): Transmitter · failed · Aug 18, 2020 · N798FD · Boeing 757222 · Trailing Flap Position Indicating System
  > TE FLAP ASYM EICAS MESSAGE. TE FLAPS STOPPED AT 2.5 DEGREES. COMPLIED WITH QRH IAW AMM 27-58-01-5. R & R THE RT TRAILING EDGE FLAP POSITION TRANSMITTER, OPS CHECKED OK, ALL INDICATIONS CHECKED NORMAL. NO HISTORY.
- [SDR FDEA201907171625](https://openairdocs.org/sdr/FDEA201907171625.md): Light · inoperative · Jul 17, 2019 · N798FD · Boeing 757222 · Emergency Lighting
  > LT LAMP FOR EMERGENCY SLIDE EXTERIOR EGRESS INOP. CHANGED BULB, NO JOY RELAMPED LT EMERGENCY SLIDE LIGHT. REF: AMM 33-51-06-2-1. OPS CHECK GOOD. MEL REMOVED. LAMP PART NUMBER 767.
- [SDR FDEA201905111027](https://openairdocs.org/sdr/FDEA201905111027.md): Light · inoperative · May 11, 2019 · N798FD · Boeing 757222 · Emergency Lighting
  > R1 DOOR ESCAPE SLIDE LIGHT INOP. RELAMPED WITH MPN 767 BULB PER AMM 33-51-06-2-1. OPS CK GOOD PER SAME.
- [SDR FDEA2018092542665](https://openairdocs.org/sdr/FDEA2018092542665.md): Frame · damaged · Sep 24, 2018 · N798FD · Boeing 757222 · Fuselage Main, Frame
  > FUSELAGE STA 1580 STR 23L-24L IS DAMAGED COMPLIED WITH FED-EX EA.# F-5310-T0340832 C P2, FUSELAGE- MAINFRAME-REPAIR OF DAMAGED FRAME DUE TO CONTAINER STRIKE, STA. 1580, STR.23L-24L. REMOVED EXISTING REPAIR AND PRODUCTION SPLICE, FABRICATED NEW REPAIR ANGLE
- [SDR FDEA201809242664](https://openairdocs.org/sdr/FDEA201809242664.md): Floorbeam · cracked · Sep 24, 2018 · N798FD · Boeing 757222 · Fuselage Main, Floor Beam
  > LT LOWER SILL STA 580 STUB BEAM CRACK, COMPLIED WITH EA F-5310-T0342453 P1. STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45. DIM OF REPAIR ANGLE 14.1/4" MADE FROM P/N: BAC1503-100274 7075-T6511, RADIUS STRAP DIM 3.1/2" X.800" MADE FR
- [SDR FDEA201806301603](https://openairdocs.org/sdr/FDEA201806301603.md): Stringer · damaged · Jun 30, 2018 · N798FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > WHILE PREFORMING SKIN REPAIR, FOUND LT STRINGER 23 AT STA 1580 DAMAGED. CUT DAMAGED SECTION OF STRINGER 23 AT STA 1580 REF SRM 53-00-03-2R. PERFORMED HFEC AFTER DAMAGE WAS CUT OUT REF NTM PT6. NO INDICATIONS NOTED. FABRICATED STRINGER REPAIR FILLER AND STRINGE
- [SDR FDEA201609193312](https://openairdocs.org/sdr/FDEA201609193312.md): Stiffener · cracked · Sep 19, 2016 · N798FD · Boeing 757222 · Fuselage Main, Bulkhead
  > LEFT WHEEL WELL AFT PRESSURE BULKHEAD INBD SIDE STIFFENER CRACKED. FABRICATED STIFFENER AND INSTALLED IAW SRM 51-40-02, DWG NR 144N2503 REV H, DWG PL 144N2503 REV BM.
- [SDR FDEA201609153266](https://openairdocs.org/sdr/FDEA201609153266.md): Skin · dented · Sep 15, 2016 · N798FD · Boeing 757222 · Trailing Edge Flaps
  > LEFT INBD MAIN FLAP LOWER SURFACE APPX 10 INCHES FROM INBD EDGE AND 3 INCHES ABOVE T/E WEDGE DENTED. REPAIRED LT INBD MAIN FLAP LOWER SURFACE BY HOT-BONDING NEW CORE & DOUBLER IAW SRM 57-53-01, FIG 1 & SRM 51-70-10-2R. REPAIR NR 3 AND SRM 51-70-10-2R REPAIR
- [SDR FDEA201609133215](https://openairdocs.org/sdr/FDEA201609133215.md): Door Frame · damaged · Sep 13, 2016 · N798FD · Boeing 757222 · Fuselage Main, Structure
  > AT THE FWD EQUIPMENT BAY DOOR 113AL CUT-OUT, FRAME BS 231.25 UPPER RADIUS DENTED & GOUGED, BL0. COMPLIED WITH EA, F-5310-T0328207, P1 FUSELAGE. MAINFRAME FORWARD ELECTRONIC EQUIPMENT COMPARTMENT, BS 231.25, BL0 FRAME DENT REPAIR. THIS IS A MAJOR REPAIR.
- [SDR FDEA201602010418](https://openairdocs.org/sdr/FDEA201602010418.md): Cable · unsecure · Feb 1, 2016 · N798FD · Boeing 757222 · Escape Slide
  > ON EXTERIOR WALK AROUND FOUND R1 DOOR WITH SLIDE RAFT HANGING OUT. REINSTALLED SLIDE RELEASE ROPE IAW AMM 25-66-01-4 & 25-66-00-5. OPERATIONS GOOD. OK FOR SERVICE.
- [SDR FDEA201510143275](https://openairdocs.org/sdr/FDEA201510143275.md): Bracket · out of adjust · Oct 14, 2015 · N798FD · Boeing 757222 · Passenger/Crew Doors
  > LEFT DOOR WILL NOT ARM FULLY, REPEAT WRITE UP. ADJUSTED RETRACTABLE DOOR STOP BRACKET & VERIFIED OPERATION OF DOOR ARMING MECHANISM TO BE CORRECT IAW AMM 52-11-20-5. REINSTALLED DOOR LINER IAW AMM 52-11-02-4. ACFT OK FOR SERVICE.
- [SDR FDEA201507092175](https://openairdocs.org/sdr/FDEA201507092175.md): Nut · unsecure · Jul 9, 2015 · N798FD · Boeing 757222 · Passenger/Crew Doors
  > LEFT HAND DOOR WILL NOT ARM. REMOVED LINER, FOUND BOLT COMPLETLY LOOSE FROM ROD END BEARING CONTROL ROD FOR RETRACTABLE DOOR (ARM INDICATOR). INSTALLED AND TORQUED THE BOLT IAW AMM 52-11-20-5, FIGURE 505. OPS CHECKED GOOD.
- [SDR FDEA201507092182](https://openairdocs.org/sdr/FDEA201507092182.md): Bolt · loose · Jul 9, 2015 · N798FD · Boeing 757222 · Passenger/Crew Doors
  > LEFT DOOR WILL NOT ARM. REMOVED LINER, FOUND BOLT COMPLETELY LOOSE FROM ROD END BEARING & CONTROL ROD FOR RETRACTABLE DOOR, ARMED INDICATOR. REINSTALLED & TORQUED BOLT.
- [SDR FDEA201507082164](https://openairdocs.org/sdr/FDEA201507082164.md): Girt Bar · dirty · Jul 8, 2015 · N798FD · Boeing 757222 · Emergency Equipment
  > ENTRY DOOR EVACUATION SLIDE VERY DIFFICULT TO ARM. REQUIRED MX ASSISTANCE TO ARM DOOR. LUBRICTED AND CLEANED GIRT BAR FOR R1 DOOR, SLIDE LIGHT ILLUMINATED, RED INDICATION DOOR EXTENDED, LEVER TURNED TO ARM POSITION. DOOR OPERATES AS DESCRIBED IN AMM
- [SDR FDEA201507082169](https://openairdocs.org/sdr/FDEA201507082169.md): Girt Bar · lack of lube · Jul 8, 2015 · N798FD · Boeing 757222 · Emergency Equipment
  > ENTRY DOOR EVACUATION SLIDE VERY DIFFICULT TO ARM. REQUIRED MX ASSISTANCE TO ARM DOOR. LUBRICATED & CLEANED GRIT BAR R1 DOOR.
- [SDR FDEA201507032141](https://openairdocs.org/sdr/FDEA201507032141.md): Unknown · malfunctioned · Jul 3, 2015 · N798FD · Boeing 757222 · Passenger/Crew Doors
  > DOOR 1R TOOK MULTIPLE ATTEMPTS TO ARM SLIDE, FELT LIKE SLIDE ARM HANDLE WAS LOCKED BUT SLIDE LIGHT OVER DOOR DID NOT ILLUMINATE WITHOUT MULTIPLE ATTEMPTS. CHECKED SECURITY & CONDITION OF MICRO SWITCHES & ASSOCIATED WIRING, GIRT BAR SLIDES & GIRT BAR SLIDE REC
- [SDR FDEA201504231380](https://openairdocs.org/sdr/FDEA201504231380.md): Brake · unknown · Apr 23, 2015 · N798FD · Boeing 757222 · Landing Gear Brake System
  > PARKING BRAKE WOULD NOT SET AT BLOCK IN. CARRIED OUT PARKING BRAKE SYS TEST IAW AMM 32-44-00-5-0, CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201503190986](https://openairdocs.org/sdr/FDEA201503190986.md): Proximity Sensor · dirty · Mar 19, 2015 · N798FD · Boeing 757222 · Escape Slide
  > ON POST FLIGHT, R1 DOOR SLIDE LIGHT DID NOT EXTINGUISH WHEN SLIDE WAS DISARMED. INSPECTED AND CLEANED R1 DOOR PROXIMITY SENSORS IAW AMM 25-66-11-2-0. CYCLED DOOR SEVERAL TIMES, DOOR ARM LIGHT OPS CHECKED GOOD.
- [SDR FDEA201409262810](https://openairdocs.org/sdr/FDEA201409262810.md): Skin Panel · damaged · Sep 26, 2014 · N798FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > INCOMING STRUCTURE INTERFERES WITH CABLE SHROUD INSTALLATION BETWEEN 1340 STRINGER 4L TO 4R. FUSELAGE SKIN REPAIR WAS ACCOMPLISHED DUE TO EFFECTING THE P TO F CONVERSION ON EA 757-5361-16-F4656 REV DATED SEPT. 16, 2014 & NR 60002686700001. THIS NR IS FOR TRA
- [SDR FDEA201409242758](https://openairdocs.org/sdr/FDEA201409242758.md): Frame · misrepaired · Sep 24, 2014 · N798FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO BAY BS 1440 STRINGER 26L. FRAME MISREPAIRED. FRAME REPAIR R & R IAW SRM 51-40-02 & DWG 146N1013. MAJOR REPAIR.
- [SDR FDEA201409042460](https://openairdocs.org/sdr/FDEA201409042460.md): Skin · dented · Sep 4, 2014 · N798FD · Boeing 757222 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERNAL SKIN, FWD LOWER EDGE DENTED. EVALUATED DENT, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01, FIG 101, DEATAIL VI. REPAIRED IAW SRM 52-30-01, REPAIR NR 4 AND EA F-5230-T0310083 TITLE; DOORS- CARGO DOOR/HYD SYS-AFT CARGO DOOR EXTERNAL SKIN
- [SDR FDEA201408142171](https://openairdocs.org/sdr/FDEA201408142171.md): Crease Beam · corroded · Aug 14, 2014 · N798FD · Boeing 757222 · Fuselage Main, Structure
  > L2 PAX DOOR LOWER CUT OUT CREASE BEAM ANGLE CORRODED. R & R INNER CHORD FROM STATION 670 - 756, LBL 60 IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, DETAIL VIII FIG 101. MAJOR REPAIR.
- [SDR FDEA201407281994](https://openairdocs.org/sdr/FDEA201407281994.md): Skin · gouged · Jul 28, 2014 · N798FD · Boeing 757222 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERNAL SKIN AFT LOWER EDGE GOUGED. REPAIRED EXTERNAL SKIN AFT LOWER EDGE OF AFT CARGO DOOR IAW SRM 52-30-01 REPAIR 4. CATEGORY B MAJOR REPAIR.
- [SDR FDEA201407221925](https://openairdocs.org/sdr/FDEA201407221925.md): Floorbeam · corroded · Jul 22, 2014 · N798FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN BS 1640 BL 0 - RBL 62, FLOORBEAM UPPER TEE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. R & R FLOORBEAM IAW SRM 51-40-02 & DWG 146N5089. MAJOR REPAIR.
- [SDR FDEA201407181853](https://openairdocs.org/sdr/FDEA201407181853.md): Seat Track · gouged · Jul 18, 2014 · N798FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 24 SEAT TRACK BS 700 - 780 DIRTY & GOUGED. REMOVED DAMAGE IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, FIG 101. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DWG I43N5080, AT RBL 24 FROM STA 700 TO STA 780. MAJOR REPA
- [SDR FDEA201407091674](https://openairdocs.org/sdr/FDEA201407091674.md): Floorbeam · corroded · Jul 9, 2014 · N798FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN FLOOR BS 365.25 RBL 71 - LBL 71, BEAM UPPER CHORD CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET III, REPAIRED FLOORBEAM UPPER CHORD AT STA 365.25 LBL13.75 - RBL 71 IAW SRM 53-00-51 FIG 201 REPAIR 8. THIS IS A CATE
- [SDR FDEA201407091673](https://openairdocs.org/sdr/FDEA201407091673.md): Seat Track · damaged · Jul 9, 2014 · N798FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, BS 418 - 440, RBL 45, NICKED, GOUGED & CORRODED. CHECKED LIMITS IAW SRM 53-00-52, FLAG NOTE G & FOUND TO BE OUT OF LIMITS. PROFILED NEW SEAT TRACK, BATCH 0002645495, PN BAC1520-792A, IAW SRM 51-40-05 & DWG 141N5131. LOCATED & DRILLED IAW SRM 51-

## 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 = 'N798FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N798FD/reports

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