# Service difficulty reports: N952FD

A list on [N952FD](https://openairdocs.org/aircraft/N952FD.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 · 71 reports

- [SDR FDEA202309071552](https://openairdocs.org/sdr/FDEA202309071552.md): Unknown · unknown · Sep 7, 2023 · N952FD · Boeing 757200 · Trailing Edge Flap Control System
  > DURING APPROACH IN TO MEM, TE FLAP DISAGREE EICAS APPEARED AND FLAPS CEASED TO MOVE WHEN MOVING FLAP HANDLE TO FLAPS 25. ACCOMPLISHED THE QRH AND LANDED WITH FLAPS 20. ***EMERGENCY DECLARED*** FIM: 27-51-00-1
- [SDR FDEA202206021361](https://openairdocs.org/sdr/FDEA202206021361.md): Skin · corroded · Jun 2, 2022 · N952FD · Boeing 757200 · Nacelle/Pylon Structure
  > RH PYLON BOLT HOLE #2 HAS DAMAGE INDICATION. CLEANED HOLE #2 BY REAMING TO.624 IAW SRM 51-40-05 AND EA # F-5730-T0368661 P1. PERFORMED ROTO-PROBE AT HOLE #2 IAW NTM 51-00-16. NO DAMAGE NOTED. WING- PLATES AND SKINS-RH WING, UPPER SKIN AND DRAG FITTING, HO
- [SDR FDEA202206011355](https://openairdocs.org/sdr/FDEA202206011355.md): Frame · cracked · Jun 1, 2022 · N952FD · Boeing 757200 · Fuselage Main, Frame
  > BS 1640 FUSELAGE FRAME WEB AT STRINGER S-14L HAS CRACK INDICATION NOTED, IN TOP INBOARD AND OUTBOARD HOLES AND BOTTOM OUTBOARD HOLE. COMPLIED WITH EA # F-5310-T0368467 P1 "FUSELAGE-MAINFRAME-FRAME 1640 AT S-14L HAS A CRACK INDICATIONS-REPAIR" MAJOR RE
- [SDR FDEA202012313224](https://openairdocs.org/sdr/FDEA202012313224.md): Slide · inoperative · Dec 31, 2020 · N952FD · Boeing 757236 · Escape Slide
  > SLIDE RAFT DEPLOYED UPON GROUND OPENING L1 DOOR FROM THE OUTSIDE. REMOVED AND REPLACED L-1 DOOR SLIDE, IAW AMM 52-11-25-5. STILL REQUIRES GIRT BAR RIG/ADJUSTMENT AND OPERATIONS CHECK. REMOVED AND INSTALLED NEW GIRT BAR ASSEMBLY ON L1 DOOR SLIDE FOR BINDING
- [SDR FDEA202011052808](https://openairdocs.org/sdr/FDEA202011052808.md): Compressor · corroded · Nov 5, 2020 · N952FD · Boeing 757236 · Turbine Engine Compressor Section
  > `#2 ENGINE COMPRESSOR CASING FWD MOST FRAME FLANGE HAS AREAS OF CORROSION AROUND THE REMOVED #2 ENGINE REF WORK CARD # 7180260-02-01 SEQ #172 AND REPLACED ENGINE REF WORK CARD # 7180260-02-02 SEQ # 173
- [SDR FDEA2020051510870](https://openairdocs.org/sdr/FDEA2020051510870.md): Skin · cracked · May 1, 2020 · N952FD · Boeing 757236 · Leading Edge Devices
  > R/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS A CRACK AT WS 594. REMOVED AND REINSTALLED #9 LEADING EDGE SLAT IAW B757 AMM 27-81-02-4, FABRICATED AND INSTALLED LOWER COVE PANEL IAW B757 SRM 51-40-02-06 AND B, DWGS. 114N4003, REV. E AND REV. B, B DWG: 114N
- [SDR FDEA2020050410870](https://openairdocs.org/sdr/FDEA2020050410870.md): Skin · cracked · May 1, 2020 · N952FD · Boeing 757236 · Leading Edge Devices
  > R/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS CRACK AT WS 594.
- [SDR FDEA2020051390839](https://openairdocs.org/sdr/FDEA2020051390839.md): Filler · corroded · Apr 29, 2020 · N952FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL.071",MAT REM.058",MAT LOSS.013" FOUND TO BE OUT OF LIMITS IAW B 75 757 SRM 53-00-51-1
- [SDR FDEA202004300839](https://openairdocs.org/sdr/FDEA202004300839.md): Filler · corroded · Apr 29, 2020 · N952FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL.071",MAT REM.058",MAT LOSS.013" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-51-1A FI
- [SDR FDEA2020043080816](https://openairdocs.org/sdr/FDEA2020043080816.md): Frame · cracked · Apr 28, 2020 · N952FD · Boeing 757236 · Fuselage Main, Frame
  > FWD CARGO PIT-R/H SIDE,FRAME 846 AT STR 22 RT. CRACKED AT FASTENER HOLE. REMOVED,FABRICATED AND INSTALLED STANCHION STUB (FRAME) ON FWD CARGO PIT R/H SIDE AT STA 846 BETWEEN STR-21R TO STR-26R IAW B 757 SRM 51-40-02-OG AND B. DWG: 143N5811, REV: -, RE
- [SDR FDEA2019032760720](https://openairdocs.org/sdr/FDEA2019032760720.md): Charger · no test · Mar 26, 2019 · N952FD · Boeing 757236 · Emergency Lighting
  > DURING POST FLIGHT MX WALKAROUND FOUND THE INTERIOR EMERGENCY EXIT LIGHT ABOVE THE L1 DOOR INOP. REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 IN POS M731, EMERGENCY LIGHT ABOVE L1
- [SDR FDEA2019032760719](https://openairdocs.org/sdr/FDEA2019032760719.md): Charger · no test · Mar 26, 2019 · N952FD · Boeing 757236 · Emergency Lighting
  > DURING POST FLIGHT MX WALKAROUND FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF THE L1 DOOR. REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 POS M731, EMERGENCY LIGHT AFT OF L1
- [SDR FDEA201902190451](https://openairdocs.org/sdr/FDEA201902190451.md): Unknown · odor · Feb 19, 2019 · N952FD · Boeing 757236 · Air Distribution System
  > AT FL 340, AIRCREW SMELLED A STRONG PUNGENT ODOR COMING FROM VENTS. IT WAS STRONG BUT NOT QUITE STRONG ENOUGH TO GO ON OXYGEN. RAN PACKS FOR 30 MINUTES AT MAX HEAT. NO UNUSUAL ODORS NOTED THROUGHOUT MAIN CARGO COMPARTMENT AND IN FLIGHT DECK. RAN BOTH ENG AT M
- [SDR FDEA2018120653432](https://openairdocs.org/sdr/FDEA2018120653432.md): Warning Message · false activation · Dec 5, 2018 · N952FD · Boeing 757236 · Passenger/Crew Doors
  > PDIS 952 52-10 5943 05DEC18 MEM FACT U LOGPAGES:2924671 MOMENTARY LEFT FORWARD ENTRY DOOR EICAS DURING CRUISE AT FL 360 PRESURIZATION NORMAL. FACT 05DEC18 05:50 MEM U COMPLIED WITH FIM 52-11 FAULT TREE 802. NO VISUAL DEFECTS NOTED. OPERAT
- [SDR FDEA201811173269](https://openairdocs.org/sdr/FDEA201811173269.md): Static Line · out of position · Nov 17, 2018 · N952FD · Boeing 757236 · Equipment/Furnishings Wiring
  > RIGHT DOOR DISARM LIGHT WILL NOT COME ON. IT INITIALLY CAME ON, BUT NOW IT STAYS OUT. DOOR DIDNT FEEL NORMAL DURING DISARM. REMOVED R1 DOOR SLIDE COVER. FOUND SLIDE STATIC LINE SQUARE KNOT INTERFERANCE WITH GIRT BAR HANDLING MECHANISM AT FORWARD GIR
- [SDR FDEA2018051571183](https://openairdocs.org/sdr/FDEA2018051571183.md): Skin · dented · May 7, 2018 · N952FD · Boeing 757236 · Leading Edge Devices
  > LARGE DENT ON TOP OF THE NR 8 SLAT WEDGE. REPAIRED THE SLAT WEDGE IAW SRM 57-43-02-2R, FIG 201, AND SRM 51-70-10-2R, REPAIR 3 AND 4, SRM 51-70-10-2R, PARAGRAPH 20, AND EA F-5750-T0339954 P1.
- [SDR FDEA201804040852](https://openairdocs.org/sdr/FDEA201804040852.md): Transmitter · failed · Apr 4, 2018 · N952FD · Boeing 757236 · Trailing Flap Position Indicating System
  > AT 13000 FT AND 220 KNOTS, CALLED FOR FLAPS 1. RECEIVED A TE FLAP ASYM ON EICAS. RECEIVED TRAILING EDGE LIGHT ON THE PANEL, FLAP ASYM OCCURRED BETWEEN FLAPS UP AND FLAPS 1 INDICATION. COMPLETED QRH AND CONTINUED TO LANDING. ACCOMPLISHED FIM 27-51 FAULT
- [SDR FDEA201711073188](https://openairdocs.org/sdr/FDEA201711073188.md): Rope · exposed · Nov 7, 2017 · N952FD · Boeing 757236 · Emergency Equipment
  > DOOR L1 HAD A PIECE OF EQUIPMENT EXPOSED AFTER CLOSING. RAMP PERSONNEL HAD US RE-OPEN DOOR TO SECURE. CALLED MX. SECURED DOOR SLIDE ROPE AND SLIDE COVER REF MM CH. 25-66-01-4. OK TO CONTINUE. OPS CHECKED NORMAL.
- [SDR FDEA201710162966](https://openairdocs.org/sdr/FDEA201710162966.md): Battery Pack · inoperative · Oct 16, 2017 · N952FD · Boeing 757236 · Emergency Lighting
  > R1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE M730 POWER SUPPLY BATTERY PACK IAW AMM 33-51-07-2, OPS CHECKED GOOD.
- [SDR FDEA201705181454](https://openairdocs.org/sdr/FDEA201705181454.md): Plug · detached · May 18, 2017 · N952FD · Boeing 757236 · Turbine Engine Oil System
  > AT FL 350, THE RT ENG OIL PRESSURE ALERT ACTIVATED. OIL QTY RAPIDLY DECREASED TO ZERO. WINDMILLED FOR 30 MINUTES. FOUND THE ENGINE CUP PLUG HAD FALLEN OUT OF THE HIGH SPEED GEARBOX REINSTALLED THE PLUG, SERVICED OIL TANK, INSPECTED CHIP DETECTORS, NO M
- [SDR FDEA201703090826](https://openairdocs.org/sdr/FDEA201703090826.md): Guard · broken · Mar 9, 2017 · N952FD · Boeing 757236 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT TEST SWITCH GUARD IS MISSING. TEST SWITCH OPS NORMAL. PLASTIC FLANGE ON SWITCH IS BROKEN AND WILL NOT REMAIN FASTENED IN PLACE. WHILE TESTING THE LIGHTS THE SWITCH FELL DOWN IN BEHIND THE SIDEWALL LINER. REMOVED AND REPLACED THE
- [SDR FDEA201612294576](https://openairdocs.org/sdr/FDEA201612294576.md): Cover · damaged · Dec 29, 2016 · N952FD · Boeing 757236 · Emergency Equipment
  > CAPTAIN`S SIDE ESCAPE ROPE COVER IS BROKEN AND LOWER LATCH HAS COME OFF. REPLACED THE ACCESS COVER IAW MM 25-61-00-0-0 PARA 2A1.
- [SDR FDEA201612094387](https://openairdocs.org/sdr/FDEA201612094387.md): Sensor · inoperative · Dec 9, 2016 · N952FD · Boeing 757236 · Door Warning System
  > SLIDE ARM LIGHTS INOP BOTH ENTRY DOORS. T/S PER FIM 25-66 TASK 802. R&R S10216 PROX SENSOR A AND S10217 PROX SENSOR B IAW AMM CH 25-66-11-2. BOTH R1 AND L1 SLIDE LIGHTS OPS CHECKS GOOD. MEL REMOVED.
- [SDR FDEA201610133611](https://openairdocs.org/sdr/FDEA201610133611.md): Unknown · odor · Oct 13, 2016 · N952FD · Boeing 757236 · Air Distribution System
  > APPROXIMATELY 20 MINUTES BEFORE COMMENCING DESCENT, A FAIRLY STRONG SMOKE ODOR OCCURRED WHICH SEEMED ELECTRICAL IN NATURE. DONNED OXYGEN MASKS AND STARTED QRH SEARCH. DID A SNIFF TEST AFTER A COUPLE MINUTES AND THE ODOR HAD DISSIPATED. CONTINUED FLIGHT
- [SDR FDEA201608222955](https://openairdocs.org/sdr/FDEA201608222955.md): Unknown · odor · Aug 22, 2016 · N952FD · Boeing 757236 · Air Distribution System
  > PASSING F360 NOTICED ELECTRICAL SMELL. PER CHECKLIST, SHUTOFF UTILITY BUSSES AND RESIRC FAN. SMELL DISAPPEARED AND PER CHECKLIST CONTINUED TO DESTINATION. PERFORMED EXAMINATION OF THE LT AIR RECIRCULATION FAN FILTERS NORMAL PER AMM 21-25-02-4. ALSO PERFOR
- [SDR FDEA201608072831](https://openairdocs.org/sdr/FDEA201608072831.md): Blower · failed · Aug 7, 2016 · N952FD · Boeing 757236 · Emergency Equipment
  > F/O EVAS BLOWER MOTOR TEST FAILED IAW WC F-2560-E0323178 A, P2, STEP 2. RT EVAS UNIT TEST PROCEDURES, RELEASED FOR SERVICE IAW MEL: 25-60-01, CATEGORY: D, EXPIRATION: 02DEC16, MEL 25-60-01. F/O EVAS UNIT REPLACED PER AMM 25-62-00-4. PERFORMED BLOWER ND BAT
- [SDR FDEA201607072310](https://openairdocs.org/sdr/FDEA201607072310.md): Lifter · broken · Jul 7, 2016 · N952FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR VERY HARD TO DISARM AND ARM. ALSO DIFFICULT TO OPEN & CLOSE. FOUND THE GIRT BAR STRIKE BRACKET BROKEN. R & R THE BROKEN L1 DOOR GIRT BAR LIFTER, 140N2754-9 AND PERFORMED DOOR GIRT BAR MECHANISM TEST IAW AMM52-11-25-5, SATISFIED. DMI CLEARED AND STI
- [SDR FDEA201605141586](https://openairdocs.org/sdr/FDEA201605141586.md): Pump · malfunctioned · May 14, 2016 · N952FD · Boeing 757236 · Engine Fuel Pump
  > FLIGHT TEST FTAM 4-66, RT ENG SHUTDOWN & RE-LIGHT FL 220 AIRSPEED 300KTS. AFTER THE NORMAL SHUTDOWN OF THE RT ENG, RELIGHT WAS ATTEMPTED. WHEN THE RT FUEL CONTROL SWITCH WAS POSITIONED FROM CUT OFF TO RUN THE SPAR, VLV OPEN & THE ENG VLV ON THE RT ENG DID NO
- [SDR FDEA201605061486](https://openairdocs.org/sdr/FDEA201605061486.md): Splice Plate · damaged · May 6, 2016 · N952FD · Boeing 757236 · Engine Mount Section
  > RIGHT ENG PYLON AFT OTBD ENG MOUNT BRACKET HAS A DING. REMOVED RT ENGINE SPLICE PLATE IAW B757 SRM 51-40-02. FABRICATED NEW SPLICE PLATE IAW SRM 51-40-05 AND 51-40-08. INSTALLED NEW SPLICE PLATE IAW SRM 51-40-02. PART MARKED IWA GMM 7-0-1001-1 PAR 7
- [SDR FDEA201507202290](https://openairdocs.org/sdr/FDEA201507202290.md): Latch · defective · Jul 20, 2015 · N952FD · Boeing 757236 · Emergency Equipment
  > PARTS FELL OFF CAPTAIN`S ESCAPE ROPE HATCH DURING PREFLIGHT. REINSTALLED LATCH COMPONENTS, HATCH LOCKED INTO PLACE. OK FOR SERVICE. MM 25-61-00-4.
- [SDR FDEA201506031690](https://openairdocs.org/sdr/FDEA201506031690.md): Collar · worn · Jun 3, 2015 · N952FD · Boeing 757236 · Passenger/Crew Doors
  > YELLOW DOOR LOCK RELEASE ON LT ENTRY DOOR IS VERY HARD TO LIFT UP WHEN CLOSING DOOR. R & R OPEN LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONS CHECKED GOOD.
- [SDR FDEA201501160205](https://openairdocs.org/sdr/FDEA201501160205.md): Light · intermittent · Jan 16, 2015 · N952FD · Boeing 757236 · Flight Compartment Lighting
  > SLIDE LIGHT ON DOOR IR ILLUMINATED INTERMITTENTLY THROUGH FLIGHT. REPLACE BULBS IAW MM 33-16-02-2. OPERATIONS CHECKED GOOD.
- [SDR FDEA201412304220](https://openairdocs.org/sdr/FDEA201412304220.md): Light · inoperative · Dec 30, 2014 · N952FD · Boeing 757236 · Emergency Lighting
  > R1 DOOR SLIDE LIGHT INOPERATIVE. SUSPECT BAD BULB. RELAMPED LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-13-00-2.
- [SDR FDEA201411023454](https://openairdocs.org/sdr/FDEA201411023454.md): Reservoir · unknown · Nov 2, 2014 · N952FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR EMER POWER RESERVOIR ASSEMBLY NEEDS TO BE REPLACED. R & R L1 DOOR EMER POWER RESERVOIR IAW AMM 52-11-30-4.
- [SDR FDEA201304280880](https://openairdocs.org/sdr/FDEA201304280880.md): Bottle · out of position · Apr 28, 2013 · N952FD · Boeing 757236 · Passenger/Crew Doors
  > DOOR ASSIST RESERVIOR GAUGE FACES IN THE UPWARD DIRECTION REQUIRING USE OF A MIRROR TO VIEW BOTTLE PRESSURE. R & R R1 EMERGENCY POWER RESERVOIR IAW AMM 52-11-30-4. ACFT OK FOR SERVICE.
- [SDR FDEA201303070509](https://openairdocs.org/sdr/FDEA201303070509.md): Door · out of adjust · Mar 7, 2013 · N952FD · Boeing 757236 · Passenger/Crew Doors
  > LEFT CREW ENTRY DOOR VERY HARD TO CLOSE. INSPECTED DOOR FOR ADJUSTMENT. DOOR OPERATES NORMAL IAW MM 52-11-00-5.
- [SDR FDEA201206282388](https://openairdocs.org/sdr/FDEA201206282388.md): Lamp · inoperative · Jun 28, 2012 · N952FD · Boeing 757236 · Emergency Lighting
  > R1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.
- [SDR FDEA201204231523](https://openairdocs.org/sdr/FDEA201204231523.md): Skin · dented · Apr 23, 2012 · N952FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > RIGHT SKIN DENTED AT BS 720 -740, STR 27. REPAIR CARRIED OUT AS PER EA F-5330-158041 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201204191491](https://openairdocs.org/sdr/FDEA201204191491.md): Strap · mismanufactured · Apr 19, 2012 · N952FD · Boeing 757236 · Horizontal Stabilizer Structure
  > HORIZONTAL STAB LEFT SIDE LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION DUE WRONG MATERIAL USED. REWORKED STRAP. REMOVED AND FABRICATED NEW RETAINING STRAP IAW DWG 182N1608, SHEET 1 REV A AND INSTALLED IAW DWG 182N1601, SHEET 2, REV. REPAIR IS CLAS
- [SDR FDEA201204191490](https://openairdocs.org/sdr/FDEA201204191490.md): Strap · mismanufactured · Apr 19, 2012 · N952FD · Boeing 757236 · Elevator Structure
  > HORIZONTAL STAB RT SIDE LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION DUE WRONG MATERIAL USED. REWORKED OF RETAING STRAP. STRAP REMOVED. NEW STRAP FABRICATED IAW DWG 182N1608, SHEET 1, REV A AND INSTALLED IAW DWG 182N1601, SHEET 2, REV. REPAIR IS C
- [SDR FDEA201204021221](https://openairdocs.org/sdr/FDEA201204021221.md): Support · chafed · Apr 2, 2012 · N952FD · Boeing 757236 · Vertical Stabilizer
  > FOUND KNIFE EDGE CHAFING ON LOWER END OF SUPPORT ON VERTICAL STAB. R & R WITH FAIRING SUPPORT FABRICIATED IAW DWG 173N1300-3, SHT 1, REV B AND INSTALLED IAW DWG 173N1300 SHT 1, REV B. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201204021218](https://openairdocs.org/sdr/FDEA201204021218.md): Skin · corroded · Apr 2, 2012 · N952FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > AFTER REMOVAL OF TCAS ANTENNA FOUND CORROSION ON SKIN AT BS 420-440 AT STRINGER 28L TO 28R. REPAIRED IAW DWG 143N3003-2, SHT 1, REV C AND DWG 143N3400, SHT 21, REV B. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201203301198](https://openairdocs.org/sdr/FDEA201203301198.md): Floor Skin · corroded · Mar 30, 2012 · N952FD · Boeing 757236 · Fuselage Floor Panel
  > CABIN DECK PLATE AT BS 1717, RBL 14 TO RBL 14.5 CORRODED. REPAIR CARRIED OUT IAW SRM 53-60-51, REPAIR 2 FIG 201, REV 105. REPAIR IS CLASSIFIED MAJOR.
- [SDR FDEA201203281157](https://openairdocs.org/sdr/FDEA201203281157.md): Angle · corroded · Mar 28, 2012 · N952FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > RT SIDE APU DOOR CUT OUT AREA THE ANGLE THAT THE NUTPLATES ARE ATTACHED TO ALONG STRINGER 2R IS CORRODED. REMOVED, FABRICATED IAW DWG 148N3152-2, SHT 1, REV- AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJO
- [SDR FDEA201203271131](https://openairdocs.org/sdr/FDEA201203271131.md): Strap · corroded · Mar 27, 2012 · N952FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > RIGHT SIDE OF APU DOOR CUTOUT AREA, BS 1825 THE APU INLET STRAP CORRODED. CORRODED STRAP REMOVED. STRAP FABRICATED IAW DWG 148N3138-8000 SHT 1, REV C, AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201203261103](https://openairdocs.org/sdr/FDEA201203261103.md): Attach Angle · corroded · Mar 26, 2012 · N952FD · Boeing 757236 · Fuselage Main, Attach Fittings
  > RT SIDE APU INLET CUTOUT, AFTER THE APU INLET REMOVAL FOUND THE INLET ATTACH ANGLE FROM STA 1793 -1825 HAS CORROSION AT STRINGER 6, RT. CORRODED RT APU INLET CUTOUT ATTACHMENT ANGLE REMOVED. REPLACED WITH ANGLE FABRICATED IAW DWG 148N3152-1, SHT 1, REV A
- [SDR FDEA201203261102](https://openairdocs.org/sdr/FDEA201203261102.md): Splice Plate · corroded · Mar 26, 2012 · N952FD · Boeing 757236 · Fuselage Main, Structure
  > APU DOOR CUT OUT AREA, RT SIDE. NUTPLATES ALONG THE FWD EDGE ARE CORRODED JUST AFT OF BS 1787 BULKHEAD FRAME. CORRODED SPLICE PLATE R & R IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SH 1REV C. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201203261097](https://openairdocs.org/sdr/FDEA201203261097.md): Skin · scratched · Mar 26, 2012 · N952FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, UNDER SHORING BS 540 - 560 BETWEEN STR 26L - 26R HAS SCRATCHES. SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201203261096](https://openairdocs.org/sdr/FDEA201203261096.md): Skin · scratched · Mar 26, 2012 · N952FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER SHORING BS 500 -520 BETWEEN STR 26L - 26R HAS SCRATCHES. DAMAGED SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV. 105. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201203221059](https://openairdocs.org/sdr/FDEA201203221059.md): Rib · corroded · Mar 22, 2012 · N952FD · Boeing 757236 · Trailing Edge Flaps
  > LEFT WING INBD T/E MAIN FLAP INBD TORQUE TUBE SUPPORT RIB LOWER AREA FOUND CORROSION. REPAIR CARRIED OUT IAW EA F-5750-158016. REPAIR IS CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N952FD/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 = 'N952FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N952FD/reports

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