# Service difficulty reports: N948FD

A list on [N948FD](https://openairdocs.org/aircraft/N948FD.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 · 175 reports

- [SDR FDEA202507171249](https://openairdocs.org/sdr/FDEA202507171249.md): Window · cracked · Jul 17, 2025 · N948FD · Boeing 757236 · Flight Compartment Windows
  > L1 WINDOW CRACK DURING CRUISE AT FL400. WINDOW STARTED ARCING AND CRACKING, RAN WINDOW DAMAGE QRH. DESELECTED L FWD WINDOW HEAT, ARCING AND CRACKING STOPPED.
- [SDR FDEA202504240642](https://openairdocs.org/sdr/FDEA202504240642.md): Floorbeam · cracked · Apr 24, 2025 · N948FD · Boeing 757236 · Fuselage Main, Floor Beam
  > INSDIE THE L/H TUNNEL AREA, AT THE FWD FACE OF THE 377 FLOOR BEAM LBL 24, THE FLOOR BEAM SUPPORT THAT RUNS FWD AND AFT IS BUCKLED AND CRACKED. FOUND DURING THE NLG INSTALL. REMOVED BROKEN STRAP, REPLACED WITH FABRICATED STRAP AND REINSTALLED ON FLOOR BEA
- [SDR FDEA202306291164](https://openairdocs.org/sdr/FDEA202306291164.md): Seat Track · damaged · Jun 29, 2023 · N948FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPART. SEAT TRACK OF 45.5 R/H BUTT LINE SECOND TRACK OF R/H SIDE @ STA. 680 IS DAMAGED. IN REF. TO WRI# 53-20/2305 ORIGINATING ITEM. REPLACED MAIN CARGO COMPARTMENT SEAT TRACK 45.5 R/H BUTT LINE SIDE STA. 640-780. REFERENCING B757 SRM 53-30-
- [SDR FDEA202306030989](https://openairdocs.org/sdr/FDEA202306030989.md): Girt Bar · damaged · Jun 3, 2023 · N948FD · Boeing 757200 · Emergency Equipment
  > MDIS 948 25-60 2270 02JUN23 EWR FACT U UPON ARRIVAL FOUND L1 DOOR AFT END OF GIRT BAR DISCONNECTED. MEL 02JUN23 06:18 EWR U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 05JUN23 "MEL 52-11-01-A: L1 DOOR INOP." MEL
- [SDR FDEA202305180894](https://openairdocs.org/sdr/FDEA202305180894.md): Skin · cracked · May 18, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STRINGER 14L STA 1400-1420 HAS 1 CRACK INDICATION NOTED AS MARKED REMOVED FASTENERS AT STRINGER 14L BETWEEN SA 1400-1420, C\W NDT NO CRACK INDICATION. INSTALLED FASENERS IAW FEDEX EA# F-5330-T0374371 P1.
- [SDR FDEA202305180893](https://openairdocs.org/sdr/FDEA202305180893.md): Skin · cracked · May 18, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STINGER 14L STA 1420-1440 HAS 1 CRACK INDICATION NOTED AS MARKED. REMOVED FASTENERS A STRINGER 14L BEWTWEEN STA 1420-1440. C\W NDT, NO CRACK INDICATION. INSTALLED FASENERS IAW FEDEX EA# F-5330-T0374371 P1.
- [SDR FDEA202305170888](https://openairdocs.org/sdr/FDEA202305170888.md): Skin · cracked · May 17, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STR 14R STA 860-880, 2 CRACK INDICATIONS NOTED AS MARKED. REMOVED FASTENERS AT STRINGER 14R BETWEN STA 860-80 (2EA). C\W NDT, NO CRACK INDICATION. INSTALLED FASTENERS IAW FEDEX EA# F-5330-T0374373 P1.
- [SDR FDEA202305170887](https://openairdocs.org/sdr/FDEA202305170887.md): Skin · cracked · May 17, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STR 14R STA 840-860, 1 CRACK INDICATION NOTED AS MARKED. REMOVED FASTENERS AT STRINGER 14R BETWEEN STA 840-860 (1EA). C\W NDT, NO CRACK INDICATION. INSTALLED FASTENERS IAW FEDEX EA# F-5330-T0374373 P1.
- [SDR FDEA202305170886](https://openairdocs.org/sdr/FDEA202305170886.md): Skin · cracked · May 17, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STR 14R STA 780-800, 3 CRACK INDICATIONS NOTED AS MARKED. REMOVED FASTENERS AT STRINGER 14R BETWEEN STA 780-800 (3EA). C\W NDT, NO CRACKS INDICATION. INSTALLED FASTENER IAW FEDEX EA F-5330-T0374373 P1
- [SDR FDEA202305170885](https://openairdocs.org/sdr/FDEA202305170885.md): Skin · cracked · May 17, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STR 14R STA 800-820, 1 CRACK INDICATION NOTED AS MARKED. REMOVED FASTENERS AT STRINGER 14R BETWEEN STA 800-820 (1EA). C\W NDT, NO CRACK INDICATION. INSTALLED FASTENERS IAW FEDEX EA# F-5330-T0374373 P1
- [SDR FDEA202305170884](https://openairdocs.org/sdr/FDEA202305170884.md): Unknown · unknown · May 17, 2023 · N948FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > STR 14R STA 520-540, 3 CRACK INDICATIONS NOTED AS MARKED. REMOVED FASTENERS AT STR 14R BETWEEN STA 520-540 (3EA) C\W NDT NO CRACKS INDICATION. INSTALLED 3 EA OVERSIZE FASTENERS IAW FEDEX EA # F-5330-T0374337 P1.
- [SDR FDEA202304220743](https://openairdocs.org/sdr/FDEA202304220743.md): Drag Fitting · unknown · Apr 22, 2023 · N948FD · Boeing 757236 · Wing, Plate/Skin
  > DURING UPPER SKIN, DRAG FITTING INSPECTION ON #2 PYLON, FOUND #4 HOLE O\B FITTING WITH POSSIBLE CRACK INDICATION AT 10 O'CLOCK POSTION AT A DEPTH OF.531". REPAIRED AT DRAG FITTING ON #2 PYLON O\B FITTING HOLE #4 IAW EA F-5730-T0374171 P1.
- [SDR FDEA202303080394](https://openairdocs.org/sdr/FDEA202303080394.md): None · none · Mar 8, 2023 · N948FD · Boeing 757200 · Emergency Equipment
  > ON POSTFLIGHT CHECK FOUND GIRT BAR LAYING ON STAIRS NOTED GIRT BAR FWD ATTACH BRACKET BROKEN. IDENTIFIED PARTS FWD L1 LIFTER ASSY MPN: 140N2754-9 CPN: 5215474 QTY: 1 RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 11
- [SDR FDEA202212072881](https://openairdocs.org/sdr/FDEA202212072881.md): Arming Lever · jammed · Dec 7, 2022 · N948FD · Boeing 757200 · Passenger/Crew Doors
  > PDIS 948 52-10 1860 07DEC22 GTF OPEN U L1 DOOR EMERGENCY SLIDE ARM LEVER IS JAMMED AND WILL NOT ARM. MEL 07DEC22 02:11 GTF U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 10DEC22 "MEL 52-11-01-A: L1 DOOR) - __ARM_
- [SDR FDEA202211152787](https://openairdocs.org/sdr/FDEA202211152787.md): Girt Bar · detached · Nov 15, 2022 · N948FD · Boeing 757236 · Emergency Equipment
  > GIRT BAR WAS FOUND LOOSE AND UNATTACHED. AMM 26-66-10-2 INSPECTECD GIRT BAR AND FITTINGS REINSTALLED PER AMM 25-66-10-2 OPERATIONAL CHECK NORMAL.
- [SDR FDEA202202250369](https://openairdocs.org/sdr/FDEA202202250369.md): Pump · none · Feb 25, 2022 · N948FD · Boeing 757200 · Hydraulic System, Main
  > JUST LEVELED IN CRUISE FLIGHT WHEN EICAS CAUTION - L HYD SYS PRESS AND RUDDER RATIO. COMPLIED WITH QRH CONTINUED TO MEM DECLARED EMERGENCY AND LANDED IN MEM. FACT 24FEB22 21:21 MEM U SUSPECT THE LH ENGINE DRIVEN PUMP SHAFT SHEARED. REMOVED THE LH EN
- [SDR FDEA202111102812](https://openairdocs.org/sdr/FDEA202111102812.md): Tire · worn · Nov 10, 2021 · N948FD · Boeing 757200 · Brake
  > #8 MLG TIRE FLAT UPON ARRIVAL AT GATE IN RIC REMOVED AND REPLACED #8 MAIN TIRE IAW AMM 32-45-01-4.
- [SDR FDEA202104271047](https://openairdocs.org/sdr/FDEA202104271047.md): Skin · cracked · Apr 27, 2021 · N948FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > CHECK FOUND FUSELAGE SKIN SURFACE CRACKED AT STA395 - STA418 S4L - S3L COMPLIED WITH EA: F-5330-T0361213 P1. TITLE: FUSELAGE - PLATES & SKINS - FUSELAGE SKIN CRACK REPAIR AT AT S-4L BETWEEN STA395 AND STA418. REPAIRED THE FUSELAGE SKIN SURFACE CRACK AT ST
- [SDR FDEA2019121753244](https://openairdocs.org/sdr/FDEA2019121753244.md): Hydraulic Line · damaged · Dec 15, 2019 · N948FD · Boeing 757236 · Hydraulic System, Main
  > AFTER LANDING L HYD QTY DROPPED TO.13 AND LO HYD SYS PRESS WARNINGS. RELEASED FOR SERVICE IAW MEL 78-31-01-01 CATEGORY C EXPIRATION 25DEC19 MEL 78-31-01-01 L IDENTIFY L OR R ENGINE THRUST REVERSER INOPERATIVE. REVERSER SECURED IN FORWARD THRUST POSITION. T
- [SDR FDEA2019080861815](https://openairdocs.org/sdr/FDEA2019080861815.md): Power Supply · no test · Aug 6, 2019 · N948FD · Boeing 757236 · Emergency Lighting
  > DURING CHECK, FOUND THE RT EMERGENCY EXIT LOCATOR SIGN LIGHT ONLY ILLUMINATIED FOR 10 SECONDS WHEN THE EMERGENCY SWITCH ON OR PERFORMED THE EMERGENCY LIGHT TEST. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY M730 IAW AMM 33-51-07-2. IAW AMM 33-
- [SDR FDEA201706011552](https://openairdocs.org/sdr/FDEA201706011552.md): Frame · dented · Jun 1, 2017 · N948FD · Boeing 757236 · Fuselage Main, Frame
  > MAIN DECK, BS 520 FRAME DENTED AT STRINGER 6R. REPAIRED THE FRAME IAW SRM 53-00-07-2R, REPAIR 3. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201605121536](https://openairdocs.org/sdr/FDEA201605121536.md): Fan · failed · May 12, 2016 · N948FD · Boeing 757236 · Air Distribution Fan
  > INFLIGHT OVHT LIGHT ILLUMINATES, EQ COOLING, EICAS MSG EQ OVHT DISPLAYS SELECTED ALT MODE & OVHT LIGHT WENT OUT. HAD ODOR IN THE COCKPIT. R & R FWD EQ SUP FAN 1 IAW MM 21-58-06-4. OPERATIONS TESTED GOOD. STATUS MSG CLEARED.
- [SDR FDEA201511163645](https://openairdocs.org/sdr/FDEA201511163645.md): Seat Belt · out of position · Nov 16, 2015 · N948FD · Boeing 757236 · Flight Compartment Equipment
  > FIRST OFFICERS LAP BELTS ARE ON THE WRONG SIDES. REPLACED NEW LAP BELT & THEN CHECKED NORMAL IAW AMM 25-11-04-4. ACFT OK FOR SERVICE.
- [SDR FDEA201511143603](https://openairdocs.org/sdr/FDEA201511143603.md): Fitting · dirty · Nov 14, 2015 · N948FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR WILL NOT DISARM. CLEANED DEBRIS FROM GIRT BAR SLIDER FLOOR FITTINGS. OPERATIONS CHECKED IAW 52-11-25-5. ACFT OK FOR SERVICE.
- [SDR FDEA201508112530](https://openairdocs.org/sdr/FDEA201508112530.md): Pump · faulty · Aug 11, 2015 · N948FD · Boeing 757236 · Hydraulic Pump (Electric/Engine), Main
  > DURING TAXI OUT WITH FLAP TRANSITION, STEERING WOULD NOT OPERATE DUPLICATED STEERING PROBLEM BY OPERATING SLATS & FLAPS & STEERING AT THE SAME TIME. HYD PRESS DROPPED BELOW THRESHOLD OF THE PRIORITY VALVE ON THE FLAP SLAT DEPRESS MODULE, TURNING STEERING SYS
- [SDR FDEA201508072512](https://openairdocs.org/sdr/FDEA201508072512.md): Cable · misrouted · Aug 7, 2015 · N948FD · Boeing 757236 · Landing Gear Steering System
  > NOSE WHEEL STEERING VERY STIFF & REQUIRES CONSTANT RT PRESS TO STAY STRAIGHT. WHEN STEERING WITH THE TILLER & ANY OTHER DEMAND ON HYD SYS IS USED STEERING FAILS COMPLETELY. REMOVED NLG WW ACCESS COVER 115 AL. REMOVED LT NLG TRUNNION PIN CABLE FAIRLEAD ASSE
- [SDR FDEA201507142270](https://openairdocs.org/sdr/FDEA201507142270.md): Slide · out of adjust · Jul 14, 2015 · N948FD · Boeing 757236 · Escape Slide
  > UNABLE TO ARM L1 DOOR. CLOSE NORMAL, UNABLE TO ARM SLIDE. ADJUSTED LI SLIDE & COVER. OPERATIONS CHECKED NORMAL IAW AMM 25-66-01.
- [SDR FDEA201506211937](https://openairdocs.org/sdr/FDEA201506211937.md): Door · inoperative · Jun 21, 2015 · N948FD · Boeing 757236 · Emergency Equipment
  > TEST FLIGHT CAPTAINS SIDE EMER ESCAPE ROPE DOOR WILL NOT LATCH. REMOVED CAPTAINS ESCAPE ROPE FOR REPAIR OF DOOR & REINSTALLED AFTER COMPLETION IAW AMM 25-61-00-4. REPAIRED CAPTAINS ESCAPE ROPE DOOR IAW AMM 25-00-00-8.
- [SDR FDEA201506191914](https://openairdocs.org/sdr/FDEA201506191914.md): Selector Valve · cracked · Jun 19, 2015 · N948FD · Boeing 757236 · Landing Gear Selector
  > TEST FLIGHT, LT HYD QTY DEPLETED TO ZERO. AFTER ACCOMPLISHING THE ALTERNATE GEAR EXTENSION PROCEDURE, DECLARED EMER & RETURNED. UPON INSPECTION OF THE MLG WW FOUND HYD LEAKING FROM MLG SELECTOR VLV. AFTER REMOVAL FOUND THE HOUSING CRACKED ON THE SELECTOR VL
- [SDR FDEA201506021679](https://openairdocs.org/sdr/FDEA201506021679.md): Bulkhead · gouged · Jun 2, 2015 · N948FD · Boeing 757236 · APU Cowling/Containment
  > APU FWD BULKHEAD GOUGED RBL 6. CUT OUT DAMAGED AREA IAW SRM 53-80-08-2R. FABRICATED REPAIR PARTS IAW SRM 53-80-08-2R & INSTALLED REPAIR PARTS IAW SRM 53-80-08-2R.
- [SDR FDEA201501050024](https://openairdocs.org/sdr/FDEA201501050024.md): Unknown · malfunctioned · Jan 5, 2015 · N948FD · Boeing 757236 · Emergency Equipment
  > ON BLOCK IN UNABLE TO DISARM L1 DOOR, WARMED DOOR. PERFORMED OPERATIONS CHECK OF SLIDE ARMING & DISARMING NUMEROUS TIMES IAW AMM 52-11-00-216-025 3 ABC. OPERATIONS CHECKED GOOD.
- [SDR FDEA201305301146](https://openairdocs.org/sdr/FDEA201305301146.md): Shear Tie · cracked · May 30, 2013 · N948FD · Boeing 757200 · Fuselage Internal Mounting Structure
  > LOWER FUSELAGE SHEAR TIE CRACKED BETWEEN STRINGER 20-21L, BS 1300. REMOVED DAMAGED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG 140N2002, REV EU AND INSTALLED SHEAR TIE IAW SRM 51-40-02 AND DWG 140N2002, REV EU.
- [SDR FDEA201303230652](https://openairdocs.org/sdr/FDEA201303230652.md): Control Column · dirty · Mar 23, 2013 · N948FD · Boeing 757236 · Control Column Section
  > FLIGHT CONTROLS BINDING ON CAPTAIN'S SIDE DURING APPROACH. PASSED CONTROL TO F/O AND F/O'S CONTROLS WERE FINE. DURING FLARE BOTH ROLL AND PITCH BOUND UP REQUIRING VERY STRONG INPUT ON CAPTAIN'S SIDE. INSPECTED CAPTAIN'S CONTROL COLUMN QUADRANT AND FOUND IT
- [SDR FDEA201302200388](https://openairdocs.org/sdr/FDEA201302200388.md): Unknown · unknown · Feb 20, 2013 · N948FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR WOULD NOT ARM AT BLOCK OUT. OPERATED L1 DOOR SEVERAL TIMES WITH NO DISCREPANCIES NOTED IAW MM 52-11-00-0.
- [SDR FDEA201302080299](https://openairdocs.org/sdr/FDEA201302080299.md): Handle · binding · Feb 8, 2013 · N948FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR DIFFICULT TO DISARM AND HARD TO CLOSE. HANDLE OPERATES NORMALLY IAW ADJUSTMENT TEST MM 52-11-00-5 AND MM 52-11-00-2. DURING GVI, FOUND EXTERNAL DOOR HANDLE LATCH SPRING VERY WEAK AS WELL AS HARDWARE IN EXTERNAL DOOR. HANDLE COVER PLATE RUBBING ON DO
- [SDR FDEA201302020255](https://openairdocs.org/sdr/FDEA201302020255.md): Girt Bar · lack of lube · Feb 2, 2013 · N948FD · Boeing 757236 · Emergency Equipment
  > LEFT ENTRY DOOR SLIDE WOULD NOT ARM. CLEANED AND LUBED L1 GIRT BAR MECHANISM, OPERATED SEVERAL TIMES OPS CHECKED GOOD AT THIS TIME IAW AMM 12-21-18-3.
- [SDR FDEA201302010248](https://openairdocs.org/sdr/FDEA201302010248.md): Bearing · failed · Feb 1, 2013 · N948FD · Boeing 757236 · Aileron Control System
  > ON TAKEOFF ROLL AT 100-110 K, AILERON CONTROL WAS UNUSUALLY STIFF WIND WAS 290/19 NO GUST. REJECTED TAKEOFF, AND PERFORMED RTO CHECKLIST IN QRH. DURING TROUBLESHOOTING, FOUND BAD BEARING AT BOTH ENDS OF INBD PCA INPUT ROD SEIZED AND FALLING APART. REMOVED
- [SDR FDEA201206182257](https://openairdocs.org/sdr/FDEA201206182257.md): Battery Pack · inoperative · Jun 18, 2012 · N948FD · Boeing 757236 · Emergency Lighting
  > RT EMERGENCY EXIT LIGHTS WILL NOT TEST. R & R RT EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.
- [SDR FDEA201201120122](https://openairdocs.org/sdr/FDEA201201120122.md): Girt Bar · binding · Jan 12, 2012 · N948FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR SLIDE ARMING LEVER WAS VERY STIFF WHEN DISARMING DOOR. OPERATED SLIDE ARMING SEVERAL TIMES. CHECKED OPS REF MM 52-11-25-5. ARMED AND DISARMED WITH NO DIFFICULTY. OK FOR SERVICE.
- [SDR FDEA201106012064](https://openairdocs.org/sdr/FDEA201106012064.md): Frame · damaged · Jun 1, 2011 · N948FD · Boeing 757236 · Fuselage Main, Frame
  > AFT LOWER CARGO, AFTER REMOVAL OF REVEAL PANEL AT STA 1380 FOUND 1 EA. ELONGATED FASTENER HOLE BETWEEN STRINGERS S26R & S27R. DAMAGED AREA REPAIRED IAW EA F-5310-146475, PART 1 (FUSELAGE BS 1380 FRAME INNER CHORD ELONGATED FASTENER HOLE AND EXTRA HOLES REPAIR)
- [SDR FDEA201105251974](https://openairdocs.org/sdr/FDEA201105251974.md): Spar · damaged · May 25, 2011 · N948FD · Boeing 757236 · Trailing Edge Flaps
  > RT INBD MAIN FLAP FRONT SPAR LOWER CHORD WITH EXISTING OVAL HOLES REPAIR COMMON TO LOWER CHORD AND LOWER SKIN AT NR 6 FLAP FAIRING ATTACH BRACKET. COMPLIED WITH EA F-5750-150712 (DOCUMENTATION OF PREVIOUS OPERATOR RT INBD MAIN FLAP FAIRING ATTACHMENT REPAIR
- [SDR FDEA201105121814](https://openairdocs.org/sdr/FDEA201105121814.md): Skin · unknown · May 12, 2011 · N948FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN WITH REPAIR AT BS 297 TO 324, BETWEEN STR 16L TO STR 18L. REPAIR REMOVED AND REPAIRED IAW EA E-5330-146479 (REPAIR ON FUSELAGE SKIN BETWEEN BS 306 TO BS 3324 AND S 16L TO S 18L - REPAIR ASSESSMENT) REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201105051755](https://openairdocs.org/sdr/FDEA201105051755.md): Skin · dented · May 5, 2011 · N948FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > LEFT STABILIZER UPPER EXTERIOR SKIN WITH EXISTING DENT (BULGING) BETWEEN RIB 13 TO RIB 14 AND STR 2 TO STR 3. REPAIR CARRIED OUT AS PER E.A. F-5510-146474 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201105051754](https://openairdocs.org/sdr/FDEA201105051754.md): Skin · dented · May 5, 2011 · N948FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > LEFT STABILISER UPPER EXTERIOR SKIN WITH EXISTING DENT (BULGING) BETWEEN RIB 13 TO 14 AND STR 1 TO 2. EXISTING REPAIR REMOVED AND DENT REPAIR CARRIED OUT AS PER E.A. F-5510-146474 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201105051753](https://openairdocs.org/sdr/FDEA201105051753.md): Skin · dented · May 5, 2011 · N948FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER UPPER AND LOWER EXTERIOR SKIN WITH EXISTING DENT. EXISTING DENT REPAIRED AS PER E.A. F-5510-146474 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201105031700](https://openairdocs.org/sdr/FDEA201105031700.md): Skin · corroded · May 3, 2011 · N948FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > HORIZONAL STAB CTR SECTION LOWER LT SPLICE STRAP SKIN AROUND RIB 2 AT S2 FOUND WITH CORROSION PRIOR TO PANEL INSTALLATION. LT SPLICE PLATE REPLACED IAW EA F-5510-149209. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201105031698](https://openairdocs.org/sdr/FDEA201105031698.md): Seat Track · misinstalled · May 3, 2011 · N948FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT STN 640 TO STN 780, LBL 24.75 IS MISMATCHED IN HEIGHT TO OTHER TRACKS. REPAIR CARRIED OUT IAW EA F-5320-149242. (SEAT TRACK HEIGHT DIFFERENCE REWORK AND CORROSION FOUND AT BS640 TO BS780, LBL45.50 TO RBL45.50. THIS IS A MAJOR ALTERATI
- [SDR FDEA201105031697](https://openairdocs.org/sdr/FDEA201105031697.md): Seat Track · out of alignment · May 3, 2011 · N948FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT STN 680 TO STN 780, LBL 45.50 IS MISMATCHED IN HEIGHT TO OTHER TRACKS. REPAIR CARRIED OUT IAW EA F-5320-149242 (SEAT TRACK HEIGHT DIFFERENCE REWORK AND CORROSION FOUND AT BS 640 TO BS 780, LBL 45.50 TO RBL 45.50). THIS IS CLASSIFIED AS
- [SDR FDEA201105031696](https://openairdocs.org/sdr/FDEA201105031696.md): Seat Track · corroded · May 3, 2011 · N948FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT STN 640 TO STN 780, RBL 24.75 IS MISMATCHED IN HEIGHT TO OTHER TRACKS. REPAIR CARRIED OUT IAW EA F-5320-149242 (SEAT TRACK HEIGHT DIFFERENCE REWORK AND CORROSION FOUND AT BS 640 TO BS780, LBL 45.50 TO RBL 45.50). THIS IS CLASSIFIED AS A
- [SDR FDEA201104291671](https://openairdocs.org/sdr/FDEA201104291671.md): Gate · corroded · Apr 29, 2011 · N948FD · Boeing 757236 · Passenger/Crew Doors
  > CABIN: DOOR 2R LOWER GATE HAS DEEP PITTING AND SURFACE CORROSION. CORRODED LOWER GATE ON R2 DOOR R & R IAW AMM 52-11-38, REV 100. REPAIR IS CLASSIFIED AS MINOR.

Next page: https://openairdocs.org/aircraft/N948FD/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 = 'N948FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N948FD/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.