# Service difficulty reports: N992FD

A list on [N992FD](https://openairdocs.org/aircraft/N992FD.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 3 · 113 reports

- [SDR FDEA202212152925](https://openairdocs.org/sdr/FDEA202212152925.md): Skin · none · Dec 15, 2022 · N992FD · Boeing 757224 · Standard Practices/Structures
  > THIS NON-ROUTINE CREATED FOR SDR/RDR TRACKING OF AIRCRAFT DAMAGE AT STATION 1681 TO 1720 STRINGERS 23R TO 26R. 0000231760: ROWLAND, GLEN J - 15-DEC-2022 23:04 ITEM WAS REPAIRED PER E.A. F-5330-T0371948 P1. SEE WO 84864 SEQ #6 FOR MAINTENANCE PERFORMED. T
- [SDR FDEA202203080438](https://openairdocs.org/sdr/FDEA202203080438.md): None · none · Mar 8, 2022 · N992FD · Boeing 757200 · Door Warning System
  > MAIN CARGO DOOR SYS STATUS MESSAGE ON ROLLOUT. OPERATED MCD SEVERAL TIMES, COULD NOT DUPLICATE WRITEUP. INSPECTED ALL 4 CAMLOCK SWITCHES FOR SECURITY AND OPERATION, ALL CHECK GOOD. THE "MN CARGO DR SYS" STATUS MESSAGE
- [SDR FDEA202201130061](https://openairdocs.org/sdr/FDEA202201130061.md): Line · leaking · Jan 13, 2022 · N992FD · Boeing 757232 · Hydraulic System, Main
  > RECEIVED R HYD QTY EICAS MESSAGE DURING CLIMB OUT FROM KBDL FOLLOWED SHORTLY BY R HYD SYS PRESS EICAS MESSAGE. CONFIRMED ZERO HYDRAULIC QUANTITY AND PRESSURE IN RIGHT SYSTEM. DIVERTED TO KIND PER GOC. COMPLIED WITH QRH. DECLARED EMERGENCY WITH KIND AIR TRA
- [SDR FDEA202112233125](https://openairdocs.org/sdr/FDEA202112233125.md): Lamp · failed · Dec 23, 2021 · N992FD · Boeing 757200 · Landing Gear Position and Warning
  > PDIS 992 32-60 8410 23DEC21 MEM OPEN U ON APPROACH AFTER GEAR WAS SELECTED DOWN THE NOSE GEAR DOWN LIGHT DID ILLUMINATE. NO GEAR UNSAFE OR OTHER INDICATIONS RECEIVED. EXECUTED A GO AROUND AND DECLARED AN EMERGENCY FOR POTENTIAL GEAR ISSUE. CO
- [SDR FDEA202112093074](https://openairdocs.org/sdr/FDEA202112093074.md): None · none · Dec 9, 2021 · N992FD · Boeing 757200 · Standard Practices/Structures
  > PERFORMED RTO AT 120 KIAS. CONSULTED QRH BRAKE COOLING CHART WHICH DIRECTED A 57 MINUTE BRAKE COOLING TIME. REF WRI 31-50 8385. PEFORMED HIGH ENERGY STOP INSP,
- [SDR FDEA202112093073](https://openairdocs.org/sdr/FDEA202112093073.md): Circuit Card · failed · Dec 9, 2021 · N992FD · Boeing 757232 · Central Warning
  > DURING TAKEOFF AT ABOUT 110KNOTS TAKEOFF, CONFIGURATION WARNING ILLUMINATED. PERFORMED RTO. FLAPS WERE SET TO 5 AND TRIM WAS IN THE GREEN. AIRCRAFT WAS PROPERLY CONFIGURED FOR TAKEOFF. R&R TAKEOFF CONFIG. WARNING CARD IAW MM 31-51-04-4. PERFORMED TAKEOF
- [SDR FDEA202108071995](https://openairdocs.org/sdr/FDEA202108071995.md): Skin · delaminated · Aug 7, 2021 · N992FD · Boeing 757232 · Leading Edge Devices
  > DISBOND FOUND 36" INBOARD OF OUTBOARD EDGE, 8" FROM AFT EDGE ON #8 SLAT UPPER SURFACE REMOVED, REPLACED, ADJUSTED AND OPS CHECKED #8 SLAT PER B757 AMM 27-81-02-4
- [SDR FDEA202108071991](https://openairdocs.org/sdr/FDEA202108071991.md): Skin · delaminated · Aug 7, 2021 · N992FD · Boeing 757232 · Leading Edge Devices
  > DISBOND INDICATION FOUND ON #4 SLAT, BOTH UPPER AND LOWER SURFACES 20 INCHES FROM INBOARD EDGE AND 6 INCHES BELOW TRAILING EDGE. REMOVED, REPLACED, ADJUSTED AND OPS CHECKED #4 SLAT IAW B757 AMM 27-81-02-4. OPS CHECK GOOD.
- [SDR FDEA202108041933](https://openairdocs.org/sdr/FDEA202108041933.md): Floorboard · damaged · Aug 4, 2021 · N992FD · Boeing 757232 · Fuselage Floor Panel
  > MAIN EQUIPMENT CENTER RH SIDE THRU ACCESS DOOR 119 FLOORBOARD EDGE IS DAMAGED ABOVE THE DOOR LATCH PLATE. FAB NEW PANEL IAW FED EX SRZ -25-005 REV R.
- [SDR FDEA202108031926](https://openairdocs.org/sdr/FDEA202108031926.md): Skin · cracked · Aug 3, 2021 · N992FD · Boeing 757232 · Passenger/Crew Doors
  > L2 INNER SKIN IS CRACKED AT LIGHTENING HOLE FLANGE JUST BELOW UPPER LATCH TORQUE TUBE, APPROXIMATELY STA 716 STR 10LH REMOVED DAMAGE IAW B757-200 SRM 52-10-01-1A, FOUND TO BE WITHIN LIMITS PER DETAIL XI, MATERIAL REMOVED.100" MAXIMUM ALLOWED.100", RESTOR
- [SDR FDEA202107301902](https://openairdocs.org/sdr/FDEA202107301902.md): Door Frame · cracked · Jul 30, 2021 · N992FD · Boeing 757232 · Fuselage Main, Structure
  > R1 DOOR CUTOUT - FWD UPPER CORNER - INNER FRAME CRACKED ACCOMPLISHED FEDEX EA # F-5310-T036230-P1: FUSELAGE - MAINFRAME - STUB FRAME STA 330 S-9R, CRACK AND DEFORMATION DAMAGE
- [SDR FDEA202107281884](https://openairdocs.org/sdr/FDEA202107281884.md): Skin · delaminated · Jul 28, 2021 · N992FD · Boeing 757232 · Trailing Edge Flaps
  > RIGHT WING INBOARD MAIN FLAP LOWER SURFACE HAS AREA OF DELAMINATION REPAIRED RIGHT WING INBOARD MAIN FLAP LOWER SKIN IAW B757 SRM 57-53-01-2R FIG 201 AND 51-70-10- 2R REPAIR 4.
- [SDR FDEA202107271873](https://openairdocs.org/sdr/FDEA202107271873.md): Seat Track · corroded · Jul 27, 2021 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 825 LBL 45 SEAT TRACK HAS MILD CORROSION REVOVED CORROSION IAW B757 -2 SRM 53-00-52-1A DETAIL I, FOUND TO BE WITHIN LIMITS, MATERIAL REMOVED.017", ORIGINAL.230", REMAINING.213". RESTORED FINISH IAW B757-2 SRM 51-20-01 AND 53-00-52-1A
- [SDR FDEA202107241850](https://openairdocs.org/sdr/FDEA202107241850.md): Skin · delaminated · Jul 24, 2021 · N992FD · Boeing 757232 · Trailing Edge Flaps
  > L/H WING OTBD FWD FLAP UPPER SURFACE HAS 4EA LOCATIONS OF DELAMINATION APPROX 70 OTBD OF THE INBD EDGE ALL CONTAINED WITHIN APPROX 20" OF EACH OTHER REPAIRED L/H WING O/B FWD FLAP UPPER SURFACE IAW B757-SRM 57-53-01-2R & 51-70-07-0G.
- [SDR FDEA202105201335](https://openairdocs.org/sdr/FDEA202105201335.md): Skin · damaged · May 20, 2021 · N992FD · Boeing 757232 · Fuselage Main, Plate/Skin
  > MAINFRAME - HOLE IN A/C FUSELAGE REPAIR COMPLY WITH E..A. F-5310-T0361682 REV NO. POS. P1 DURING LOADING OPERATIONS AT IND, A LOADER STRUCK THE FUSELAGE BELOW THE MAIN CARGO DOOR AND BOLT PUSHED A HOLE INTO THE FUSELAGE WITH A CORRESPONDING DENT IN THE
- [SDR FDEA202105151313](https://openairdocs.org/sdr/FDEA202105151313.md): Skin · damaged · May 15, 2021 · N992FD · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING LOADING OPERATIONS AT IND, A LOADER STRUCK THE FUSELAGE BELOW THE MAIN CARGO DOOR AND BOLT PUSHED A HOLE INTO THE FUSELAGE WITH A CORRESPONDING DENT IN THE IMPACT AREA (STA 603.5 AND STRINGER 19L) JUST ABOVE A SKIN SPLICE NEAR THE AFT CORNER OF THE MC
- [SDR FDEA202003120557](https://openairdocs.org/sdr/FDEA202003120557.md): Sensor · failed · Mar 12, 2020 · N992FD · Boeing 757232 · Door Warning System
  > L FWD ENT DOOR EICAS MSG DISPLAYED IN FLT DURING CRUISE AT FL 360 INTERMITTENTLY THEN EXTINGUISHED ON DECENT. R/R L1 DOOR LOCKED SENSOR S10094 - REF M/M 52
- [SDR FDEA2019101762672](https://openairdocs.org/sdr/FDEA2019101762672.md): Frame · corroded · Oct 16, 2019 · N992FD · Boeing 757232 · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT - CORROSION ON UPPER FLANGE OF FRAME AT BS 700 RBL1 COMPLIED WITH FEDEX EA # F-5310-T0349986 P1. FUSELAGE - MAINFRAME - STA 700 FRAME REPAIR BETWEEN STRINGERS S-28R AND S-28L
- [SDR FDEA2019101402619](https://openairdocs.org/sdr/FDEA2019101402619.md): Floor Support · corroded · Oct 10, 2019 · N992FD · Boeing 757232 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENTM CORROSION ON INTERCOSTAL BS 655 RBL 25. REMOVED INTERCOSTAL FWD CARGO COMP BS 655 RBL 25. EVALUATED INTERCOSTAL FOUND OUT OF LIMITS IAW B757 SRM 51-40-02-0G AND 53-00-04-1A FIG 101 DET II. FORMED, TRIMMED, LOCATED, DRILLED AND I
- [SDR FDEA2019101092543](https://openairdocs.org/sdr/FDEA2019101092543.md): Skin · gouged · Oct 9, 2019 · N992FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE HAD A DENTED AREA AT BS 513, BETWEEN STRINGERS 28L AND 29L. EVALUATED DENTED AREA AND FOUND THE AREA TO HAVE TWO GOUGES IAW IAW SRM 51-10-02-0G, AND BLENDED AREA AND FOUND MINIMUM THICKNESS REMAINING OF SKIN AREA.030. FOUND TO BE OUT OF LIM
- [SDR FDEA201910032417](https://openairdocs.org/sdr/FDEA201910032417.md): Skin · corroded · Oct 3, 2019 · N992FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > BOTTOM EXT FUSELAGE SKIN UPPER SURFACE HAS 2 SQUARE INCHES OR CORROSION AND BULGING LOCATED AT THE MAIN E&E BAY DOOR 119BL FWD CUTOUT BETWEEN 2EA STOP FTGS. COMPLIED WITH EA F-5330-T0349870, P1.
- [SDR FDEA2019100322395](https://openairdocs.org/sdr/FDEA2019100322395.md): Shear Tie · corroded · Oct 2, 2019 · N992FD · Boeing 757232 · Fuselage Internal Mounting Structure
  > AFT CARGO SHEAR TIE BS 1460 CORRODED. FOUND WITH 100% MATERIAL LOSS. OUT OF LIMITS IAW SRM 53-00-07-1A, FIG 101, DET II, REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 146N1014, REV D.
- [SDR FDEA201909272362](https://openairdocs.org/sdr/FDEA201909272362.md): Floorbeam · cracked · Sep 27, 2019 · N992FD · Boeing 757232 · Fuselage Main, Floor Beam
  > STUB FLOORBEAM STA. 580 LBL 45.5 CRACK AT AFT INNER RADIUS COMPLIED WITH FEDEX EA # F - 5310-T0349768 P1, TITLE: STUB FLOOR BEAM STA. 580 LBL 45.5 CRACK AT AFT INNER RADIUS.
- [SDR FDEA2019060311201](https://openairdocs.org/sdr/FDEA2019060311201.md): Fuse · leaking · May 31, 2019 · N992FD · Boeing 757232 · Brake Anti-Skid Section
  > AFTER BLOCK IN. RIGHT HYDRAULIC LEAK. LOST RIGHT HYDRAULIC QUANITY REMOVED AND REPLACED #4 BRAKE NORMAL ANTISKID MANIFOLD BRAKE FUSE REF AMM 32-42-03-4-0. LEAK AND OPS CK GOOD.
- [SDR FDEA2018110763110](https://openairdocs.org/sdr/FDEA2018110763110.md): Target · out of limits · Nov 6, 2018 · N992FD · Boeing 757232 · Door Warning System
  > L AFT EMERGENCY DOOR EICAS LIGHT. RAN QRH. GOOD PRESSURE, CONTINUED. WITH DOOR CLOSED FOUND GAP BETWEEN SENSOR AND TARGET OUT OF LIMITS. ADJUSTED TARGET IAW AMM 57-71-00-5. OPS CHECKS
- [SDR FDEA2018100282739](https://openairdocs.org/sdr/FDEA2018100282739.md): Collar · not reported · Sep 28, 2018 · N992FD · Boeing 757232 · Passenger/Crew Doors
  > L1 DOOR WILL NOT CLOSE, GUST LOCK BUSHING SEIZED UP, POSSIBLE CRACKED OR TOOTH BROKE OFF. REPLACED L1 DOOR HOLD OPEN LOCK COLLAR PER MM 52-11-08-8. OPS CHECK NORMAL. A/C OK FOR SERVICE. P/N REPLACED WAS 654N0244-7, NO SERIAL NUMBER ON PART.
- [SDR FDEA201802270501](https://openairdocs.org/sdr/FDEA201802270501.md): Light · inoperative · Feb 27, 2018 · N992FD · Boeing 757232 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSY IAW MM 33-51-06-2-1. OPS CHECKED GOOD.
- [SDR FDEA201802270500](https://openairdocs.org/sdr/FDEA201802270500.md): Battery Pack · inoperative · Feb 27, 2018 · N992FD · Boeing 757232 · Emergency Lighting
  > L1 DOOR INTERIOR EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51-07-2-0.
- [SDR FDEA201712293472](https://openairdocs.org/sdr/FDEA201712293472.md): Gust Lock · out of adjust · Dec 29, 2017 · N992FD · Boeing 757232 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK IS VERY STIFF TO OPERATE. IAW AMM: 52-11-08-8, ADJUSTED THE L1 DOOR HOLD OPEN LOCK AMM 52-11-08-4-0 AND ALIGNED THE PAX DOOR HOLD OPEN LOCK IAW AMM 52-11-08-8-0. OPS CHECKED NORMAL.
- [SDR FDEA201712273452](https://openairdocs.org/sdr/FDEA201712273452.md): Light · unknown · Dec 27, 2017 · N992FD · Boeing 757232 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. COULD NOT DUPLICATE PROBLEM. PERFORMED EMERGENCY LIGHT TEST AND LIGHT OP'S CHECKED GOOD IAW MM 33-51-00-5.
- [SDR FDEA201712273451](https://openairdocs.org/sdr/FDEA201712273451.md): Connector · not seated · Dec 27, 2017 · N992FD · Boeing 757232 · Light System Wiring
  > RESEATED EMERGENCY EXIT SIGN AND PERFORMED EMERGENCY LIGHT TEST AND LIGHT OP'S CHECKED GOOD IAW 757 MM 33-51-00-5.
- [SDR FDEA201710102898](https://openairdocs.org/sdr/FDEA201710102898.md): Seat Track · cracked · Oct 10, 2017 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > ON REMOVAL OF THE SEAT TRACK FROM BS 440 TO 640, RBL 45 FOUND CRACKED. FABRICATED A NEW SEAT TRACK IAW SRM 51-40-05-0G AND DWG 143N5080, REV A.
- [SDR FDEA201710022813](https://openairdocs.org/sdr/FDEA201710022813.md): Frame · cracked · Oct 2, 2017 · N992FD · Boeing 757232 · Fuselage Main, Frame
  > BS 1640 FRAME AT LONGERON 14L IS CRACKED. REPAIRED IAW EA F-5310-T0335764, P1.
- [SDR FDEA201710012850](https://openairdocs.org/sdr/FDEA201710012850.md): Crease Beam · corroded · Oct 1, 2017 · N992FD · Boeing 757232 · Fuselage Main, Structure
  > BS 370 - 377, RBL 64, LOWER SURFACE OF CREASE BEAM INBD ANGLE HAS SIGNS OF CORROSION. REMOVED THE CREASE BEAM IAW SRM 51-10-02. OUTT OF LIMITS IAW SRM 53-30-13-1A. REMOVED THE WEB IAW SRM 51-40-02. FABRICATED A NEW WEB IAW DWG 141N8322, REV K. INSTALLED T
- [SDR FDEA201709252719](https://openairdocs.org/sdr/FDEA201709252719.md): Frame · damaged · Sep 25, 2017 · N992FD · Boeing 757232 · Fuselage Main, Frame
  > STA 231 FRAME HAS A HOLE IN IT. REPAIRED 231 FRAME IAW SRM 53-00-07-2R REP 7. PERFORMED SATISFACTORY OPS CHECK OF DOOR SWITCH IAW AMM 52-71-00-5.
- [SDR FDEA201707212015](https://openairdocs.org/sdr/FDEA201707212015.md): Spring · failed · Jul 21, 2017 · N992FD · Boeing 757232 · Emergency Equipment
  > WHEN CLOSING L1 DOOR, EMERGENCY SLIDE GIRT BAR FELL OUT FOUND LEAF SPRINGS BAD. REMOVED AND REPLACED GIRT BAR ASSY IAW MM 25-66-10-2. DOOR SLIDE ARMS AND DISARMS NORMAL.
- [SDR FDEA201706071584](https://openairdocs.org/sdr/FDEA201706071584.md): Girt Bar · damaged · Jun 7, 2017 · N992FD · Boeing 757232 · Emergency Equipment
  > AFTER PREFLIGHT WAS COMPLETED, COULD NOT CLOSE L1 DOOR. FOUND GIRT BAR HANGING FROM BOTTOM OF DOOR. REMOVED AND REPLACED THE L1 GIRT BAR ASSY IAW AMM 25-66-10-2. DOOR ARMS & DISARMS GOOD.
- [SDR FDEA201603090911](https://openairdocs.org/sdr/FDEA201603090911.md): Collar · damaged · Mar 9, 2016 · N992FD · Boeing 757232 · Passenger/Crew Doors
  > AIRCRAFT L1 DOOR WILL NOT CLOSE. GUST LOCK DOESN’T OPEN, SO DOOR WON’T OPEN. R & R L1 DOOR GUST LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONAL CHECK OF L1 ENTRY DOOR NORMAL, RII PROCEDURES COMPLIED WITH.
- [SDR FDEA201503040650](https://openairdocs.org/sdr/FDEA201503040650.md): Arm · dirty · Mar 4, 2015 · N992FD · Boeing 757232 · Emergency Equipment
  > MAIN CABIN R1 EXIT DOOR SLIDE ARM POPPED OUT. INDICATOR INTERMITTENTLY STICKS IN & OUT OF VIEW. FOUND DEBRIS IN UPPER PORTION OF RETRACTABLE DOOR CUT OUT CAUSING INDICATOR NOT TO EXTEND PROPERLY. CLEANED CUT OUT AREA OF DEBRIS & INDICATOR WORKS CORRECTLY.
- [SDR FDEA201407222347](https://openairdocs.org/sdr/FDEA201407222347.md): Switch · tripped · Jul 22, 2014 · N992FD · Boeing 757232 · Leading Edge Slat Control System
  > LE SLAT ASM EICAS MSG WHILE RETRACTING FLAPS DURING TAKEOFF. COMPLIED WITH QRH, LANDED NOTICED NO ROLLING OR CONTROL DIFFICULTY. LT ALTN FLAP & FLAPS AT 20 DEGREES. FOUND UPPER EICAS WITH AMBER LE SLATS ASYM MSG DISPLAYED BUT NO LOWER EICAS OR SELECTED EICA
- [SDR FDEA201406021281](https://openairdocs.org/sdr/FDEA201406021281.md): Wedge · dented · Jun 2, 2014 · N992FD · Boeing 757232 · Leading Edge Devices
  > HAIL DAMAGE NR 2 SLAT TE WEDGE. ACCOMPLISHED EX EA F-5750-T0308596 PT1 FLIGHT CONTROLS, LE SLATS & FLAPS, NR 2 SLAT TE WEDGE REPAIR.
- [SDR FDEA201406021280](https://openairdocs.org/sdr/FDEA201406021280.md): Wedge · dented · Jun 2, 2014 · N992FD · Boeing 757232 · Leading Edge Devices
  > HAIL DAMAGE NR 4 SLAT TE WEDGE. ACCOMPLISHED EA F-5750-T0308597 PT 1 FLIGHT CONTROL, LE SLATS & FLAPS NR 4 SLAT TE WEDGE REPAIR.
- [SDR FDEA201406021279](https://openairdocs.org/sdr/FDEA201406021279.md): Skin · dented · Jun 2, 2014 · N992FD · Boeing 757232 · Trailing Edge Flaps
  > HAIL DAMAGE, LT WING MAIN FLAP UPPER SURFACE INBD SIDE HAS 2 DENTS. ACCOMPLISHED EA F-5750-T0308600 PT1 WINGS, LT WING INBD MAIN FLAP UPPER SKIN REPAIR.
- [SDR FDEA201406021278](https://openairdocs.org/sdr/FDEA201406021278.md): Skin · dented · Jun 2, 2014 · N992FD · Boeing 757232 · Trailing Edge Flaps
  > HAIL DAMAGE LT OTBD FLAP HAS 2 DENTS DELAMINATED. ACCOMPLISHED EA F-5750-T0308601 PT 1, WINGS, LT WING OTBD MAIN FLAP UPPER SKIN REPAIR.
- [SDR FDEA201405271240](https://openairdocs.org/sdr/FDEA201405271240.md): Skin · dented · May 27, 2014 · N992FD · Boeing 757232 · Trailing Edge Flaps
  > HAIL DAMAGE LT WING INBD AFT FLAP UPPER SURFACE. COMPLIED WITH EA F-5750-TO308549 SEE COPY ATTACHED LT WING AFT FLAP UPPER SKIN REPAIR RSC.
- [SDR FDEA201405151039](https://openairdocs.org/sdr/FDEA201405151039.md): Panel · defective · May 15, 2014 · N992FD · Boeing 757232 · Passenger/Crew Doors
  > RIGHT ENTRY DOOR ARMED SLIDE PLACARD REMAINS IN DISARMED POSITION WHEN SLIDE WAS ARMED. PLACARD HAS TO BE BE MANUALLY MOVED TO THE ARMED POSITION. FOUND ARMED POP OUT INDICATOR RUBBING CUT OUT PANEL, REMOVED EXCESS FROM PANEL. OPERATIONS CHECKED DOOR ARMING
- [SDR FDEA201403190531](https://openairdocs.org/sdr/FDEA201403190531.md): Wire · open · Mar 19, 2014 · N992FD · Boeing 757232 · Emergency Lighting
  > L1 SLIDE EMERGENCY LIGHT INOPERATIVE. FOUND OPEN GROUND WIRE W3532-0001-20. TERMINATED WIRE AT GROUND POINT GD478-DC REF AWD 33-51-12. EMERGENCY LIGHT SYSTEM TESTS NORMAL IAW MM 33-51-00-5.
- [SDR FDEA201401140096](https://openairdocs.org/sdr/FDEA201401140096.md): Sign · inoperative · Jan 14, 2014 · N992FD · Boeing 757232 · Emergency Lighting
  > L1 EMERGENCY EXIT LIGHT SIGN INOPERATIVE. RELEASED FOR SERVICE PER MEL 33-51-01-01 CATEGORY D EXPIRATION 4MAY14.
- [SDR FDEA201211133990](https://openairdocs.org/sdr/FDEA201211133990.md): Lamp · inoperative · Nov 13, 2012 · N992FD · Boeing 757232 · Escape Slide
  > SLIDE ARMED LIGHT FOR L1 DOOR IS INOPERATIVE, RELAMPED L1 "SLIDE" LIGHT. SLIDE LIGHT ILLUMINATES NORMAL, ACFT OK FOR SERVICE.
- [SDR FDEA201203211039](https://openairdocs.org/sdr/FDEA201203211039.md): Handle · separated · Mar 21, 2012 · N992FD · Boeing 757232 · Landing Gear Brake System
  > ON COMPLETION OF PUSH BACK, PARKING BRAKE HANDLE CAME OFF, UNABLE TO ENGAGE PARKING BRAKE. RECONNECTED HANDLE BY TIGHTENING SET SCREWS, PERFORMED WORK IAW SMP.

Next page: https://openairdocs.org/aircraft/N992FD/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 = 'N992FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N992FD/reports

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