# Service difficulty reports: N995FD

A list on [N995FD](https://openairdocs.org/aircraft/N995FD.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 · 111 reports

- [SDR FDEA202610091507](https://openairdocs.org/sdr/FDEA202610091507.md): Shutoff Valve · faulted · Oct 9, 2026 · N995FD · Boeing 7572Q8 · Cabin Pressure Control System
  > AT FL350, GOT MASTER WARNING CABIN ALTITUDE, WENT TO 12,000FT. (EMERGENCY DECLARED) R & R LT PACK FLOW CONTROL AND SHUTOFF VALVE. OPS CHECK, LEAK CHECK GOOD.
- [SDR FDEA202608281244](https://openairdocs.org/sdr/FDEA202608281244.md): Extinguisher · discharged · Aug 28, 2026 · N995FD · Boeing 7572Q8 · Fire Bottle, Fixed
  > WHEN ACFT WAS TOWED INTO GATE AND MX INSP. FOUND NR 1 CARGO FIRE BOTTLE DISCHARGED. AMM: 26-23-02-4 R & R NR 1 CARGO FIRE BOTTLE AND TEST IAW MM 26-23-02-4 WITH SAT RESULTS, OK FOR SERVICE.
- [SDR FDEA202608271238](https://openairdocs.org/sdr/FDEA202608271238.md): Smoke Detector · inoperative · Aug 27, 2026 · N995FD · Boeing 7572Q8 · Smoke Detection
  > ON CLIMBOUT FROM LFT-MEM WE HAD A MAIN CARGO MIDDLE SMOKE DETECTOR LIGHTS 2,3,4 ILLUMINATE. NO OTHER INDICATIORS OF SMOKE OR FIRE, DECLARED EMERGENCY, RETURNED TO LFT RAN QRC & QRH STOPPED ON RUNWAY, EMERGENCY CREW SAW AND DETECTED NO FIRE OR SMOKE INDICA
- [SDR FDEA202409101278](https://openairdocs.org/sdr/FDEA202409101278.md): Bottle · empty · Sep 10, 2024 · N995FD · Boeing 7572Q8 · Crew Oxygen System
  > DURING B-CHECK FOUND AFT O2 BOTTLE AT ZERO PRESSURE. REPLACED BOTTLE PER AMM ON NON ROUTINE 8, PERFORMED MVP ON WRI 0000813271. REMOVED AND REPLACED AFT OXYGEN BOTTLE PER 757 AMM 35-11-30-4-99. AC OK FOR SERVICE
- [SDR FDEA202407060961](https://openairdocs.org/sdr/FDEA202407060961.md): Ground Stud · unsecure · Jul 6, 2024 · N995FD · Boeing 7572Q8 · Light System Wiring
  > EMERGENCY LIGHTS WON'T TEST FROM NOSE GEAR SWITCH S10035. CK OK FROM TEST SWITCH ABOVE L1 DOOR. CHECKED FOR POWER AND GROUND AT SWITCH S10035. POWER GOOD AT TERMINAL 2 BUT FOUND NO GROUND ON TERMINAL 1. FOUND LOOSE CONNECTION AT GROUND STUD GD29-DC. SECU
- [SDR FDEA202407020912](https://openairdocs.org/sdr/FDEA202407020912.md): Battery Pack · no test · Jul 2, 2024 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > EMERGENCY LIGHTS WON'T TEST USING ANY/ALL SWITCHES. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY M 730 AND M731 OPS CHECK GOOD REF AMM 33-51-07- 2. PART REMOVED IS RADIANT POWER CORP BATTERY ASSEMBLY PART NUMBER 2103-1A.
- [SDR FDEA202110082491](https://openairdocs.org/sdr/FDEA202110082491.md): Skin · unknown · Oct 8, 2021 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > DURING THE ACCOMPLISHMENT OF THE PREVENTATIVE DOUBLER INSTALLATION PER EO F- 5330-E0341230-P12, IT WAS NOTED THAT HAECO MX COULD NOT COMPLY WITH WORK INSTRUCTIONS AS DIRECTIED WITH IN THE EO AND ASSOCIATED INSTALLATION DRAWING DUE TO ACFT CONFIGURATION.
- [SDR FDEA202110032456](https://openairdocs.org/sdr/FDEA202110032456.md): Flap · delaminated · Oct 3, 2021 · N995FD · Boeing 757* · Trailing Edge Flap Control System
  > INBOARD FLAP LOWER INBOARD PANEL IS DELAMINATED. REPAIRED I/B FLAP LOWER I/B PANEL WITH PERMANENT REPAIR IAW B757 SRM 57-53-01-2R FIG 201 SHEET 2 AND 51-70-10-2R.
- [SDR FDEA202110022446](https://openairdocs.org/sdr/FDEA202110022446.md): Web · damaged · Oct 2, 2021 · N995FD · Boeing 757* · Fuselage Structure (General)
  > L1 DOOR CUTOUT, INNER WEB AT SNUBBER LOCATION IS DAMAGED DAMAGE BLENDED ON L1 DOOR CUTOUT WEB IAW B757-200 SRM 51-10-02. ORIGINAL THICKNESS OF WEB IS.050, REMAINING THICKNESS IS.025, LOSS OF MATERIAL IS.025 FOUND TO BE OUT OF LIMITS IAW BAC DWG 141N
- [SDR FDEA202109292431](https://openairdocs.org/sdr/FDEA202109292431.md): None · none · Sep 29, 2021 · N995FD · Boeing 7572Q8 · Elevator Structure
  > LEFT ELEVATOR LOWER INBOARD SURFACE HAS TWO DENTS REPAIRED LEFT ELEVATOR LOWER INBOARD SURFACE IAW B757 SRM 55-20-01-2R AND 51-70- 05-0G PARA. 5.B.
- [SDR FDEA202109272423](https://openairdocs.org/sdr/FDEA202109272423.md): None · delaminated · Sep 27, 2021 · N995FD · Boeing 757* · Wing, Control Surfaces
  > LEFT WING, OUTBOARD FLAP, AFT FLAP, 6 - INCHES FROM INBOARD EDGE POSSIBLLY DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIR AND REPAIRED LEFT WING OUTBOARD FLAP AFT FLAP 6" FROM INBOARD EDGE IAW B757 SRM 57-53-01-2R1 FIG 201 SHEET 5.
- [SDR FDEA202109222356](https://openairdocs.org/sdr/FDEA202109222356.md): Skin · dented · Sep 22, 2021 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER EXTERIOR SURFACE AT STA 1730 HAS 3 EA PROTRUDING DENTS MEASURED DENTS ON FUSELAGE LOWER EXTERIOR SURFACE SKIN AT STA 1730, DENT1: A=.300 AND Y=.004 =.300/.004= 75, DENT2: A=.301 Y=.002 A/Y= 150 AND DENT 3: A=.350 Y=.022=15, DENT #3 IS
- [SDR FDEA202109202351](https://openairdocs.org/sdr/FDEA202109202351.md): Seat Track · damaged · Sep 20, 2021 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK SECTION IS DAMAGED @ STA 580, LBL 45 REPAIRED SEAT TRACK SECTION FROM STA 530 - STA 610, LBL 45 IAW FEDEX EA # F-5310-T0364284-P1, RELEASED OCT 05, 2021, TITLED " FUSELAGE - MAINFRAME - SEAT TRACK, STA 580, LBL 45, DAMAGED SCALLOP"
- [SDR FDEA202109202349](https://openairdocs.org/sdr/FDEA202109202349.md): Skin · chafed · Sep 20, 2021 · N995FD · Boeing 7572Q8 · Trailing Edge Flaps
  > RIGHT WING, OUTBD MAIN FLAP, CENTER LEADING EDGE SKIN HAS 2EA WEAR SPOTS. REPAIRED RH WING OB MAIN FLAP IAW EA F-5750-T0364593-P1,
- [SDR FDEA202004230776](https://openairdocs.org/sdr/FDEA202004230776.md): Control Panel · malfunctioned · Apr 23, 2020 · N995FD · Boeing 7572Q8 · Smoke Detection
  > WHILE FINISHING PRE-FLIGHT WITH 'BEFORE START CHECKLIST' COMPLETED 'TO-THE-LINE' THE AFT PEDESTAL FIRE/OVERHEAT FAIL LIGHT WAAS ILLUMINATING INTERMITTENTLY. THEN WE SMELLED AN ACID BURNING SMELL FOLLOWED BY A VISUALLY VERIFIED FIRE (FLAMES) INSIDE THE AFT
- [SDR FDEA202004230777](https://openairdocs.org/sdr/FDEA202004230777.md): Test Panel · contaminated · Apr 23, 2020 · N995FD · Boeing 7572Q8 · Fire Detection
  > AFT PEDESTAL FIRE/OVERHEAT FAIL LIGHT ILLUMINATED INTRMITNLY. SMELLED SMOKE VISUALLY VERIFIED FIRE INSIDE THE AFT PEDESTAL. SHUT DOWN PWR TO AC. AIRCRAFT MX AND ARFF. FOUND BURNS ON FAIL/RESET SWITCH PANEL, LOOKS TO HAVE LIQUID SPILL RESIDUALS ON IT.
- [SDR FDEA202004080718](https://openairdocs.org/sdr/FDEA202004080718.md): Bottle · failed · Apr 8, 2020 · N995FD · Boeing 7572Q8 · Passenger/Crew Doors
  > L1 DOOR ASSIST BOTTLE HAS BEEN DEPLETED REMOVED REPLACED L-1 DOOR EMERGENCY POWER RESERVOIR PER BOEING AMM 52-11-30-4. A/C OK FOR SERVICE AT THIS TIME.
- [SDR FDEA2020012430213](https://openairdocs.org/sdr/FDEA2020012430213.md): Probe · failed · Jan 23, 2020 · N995FD · Boeing 7572Q8 · Pitot/Static System
  > RT AUX PITOT EICAS AND LIGHT 15 MINS INTO FLIGHT. ON DECENT WENT INTO ICING CONDITIONS AFTER CONSULTATION WITH MOCC THAT THIS WOULD BE ACCEPTABLE. GOT EICAS IAS DISAGREE, RUDDER RATIO, MACH TRIM EICAS WHEN IN IMC. RECORD EVENT PRESSED SEEMED TO COME BACK WH
- [SDR FDEA2019122313276](https://openairdocs.org/sdr/FDEA2019122313276.md): Skin · chafed · Dec 21, 2019 · N995FD · Boeing 7572Q8 · Trailing Edge Flaps
  > REWORK REQUIRED OF EA F-5750-T0351491 PT1 STEP 3. REPAIR ACCOMPLISHED IAW SRM 57-53-01-2R REPAIR 2 AND EA F-5750-T0351491 A P1 WING - FLIGHT SURFACES. RT INBOARD MAIN FLAP LEADING EDGE SKIN REPAIR.
- [SDR FDEA2019121303220](https://openairdocs.org/sdr/FDEA2019121303220.md): Doubler · worn · Dec 10, 2019 · N995FD · Boeing 7572Q8 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP HAS WORN MARKED IN MULTIPLES AREAS OF LEADING EDGE SURFACE. REMOVED DAMAGE ON RT WING I/B FLAP L/E O/B SIDE AND FOUND DAMAGE AT SKIN PLATE DOUBLER OF EXISTING REPAIR AND OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101 DET VI. FORMED, LOCATE
- [SDR FDEA2019120973207](https://openairdocs.org/sdr/FDEA2019120973207.md): Skin · chafed · Dec 7, 2019 · N995FD · Boeing 7572Q8 · Trailing Edge Flaps
  > CHAFED MARK SHOWING AT RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLIED WITH EA F-5750-T0351338 P1 TITLE: WING - FLIGHT SURFACE - RT OUTBOARD MAIN FLAP LEADING EDGE SKIN REPAIR. BLENDED AREA FOUND OUT OF LIMITS L/E AREA IAW SRM 57-53-01-1A FIG 101 DET VI. FAB
- [SDR FDEA2019120653191](https://openairdocs.org/sdr/FDEA2019120653191.md): Seat Track · corroded · Dec 5, 2019 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN STA 1180 - 1200 BL0 SEAT TRACK FLANGE CORRODED. COMPLIED WITH EA F-5310-T0351165 P1. TITLE FUSELAGE - MAINFRAME - BL 0 SEAT TRACK SPLICE REPAIR BETWEEN STA 1220 AND STA 1240.
- [SDR FDEA2019120653190](https://openairdocs.org/sdr/FDEA2019120653190.md): Skin · worn · Dec 5, 2019 · N995FD · Boeing 7572Q8 · Trailing Edge Flaps
  > RIGHT WING LEADING EDGE WORN MARKED AT INBOARD SIDE, OUTBD FLAP INBD L/E. BLENDED AREA AT RIGHT WING LEADING EDGE OF O/B FLAP IB SIDE, INBD L/E FOUND AREA OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101 NOTE S. FABRICATED, LOCATED AND DRILLED DOUBLER RT WING L/E O
- [SDR FDEA201912043173](https://openairdocs.org/sdr/FDEA201912043173.md): Floorbeam · cracked · Dec 4, 2019 · N995FD · Boeing 7572Q8 · Fuselage Main, Floor Beam
  > CRACK FLOORBEAM T CAP STA 580 LBL 45.5. COMPLIED WITH EA F-5310-T0351069 P1. TITLE: FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.
- [SDR FDEA201912043172](https://openairdocs.org/sdr/FDEA201912043172.md): Web · corroded · Dec 4, 2019 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > MAIN DECK BETWEEN STA 1640 - 1681 RBL 50 WEB CORRODED ON TOP AND UNDER NUT PLATE. REMOVED CORROSION IN AREA AT MAIN DECK BETWEEN STA 1640 - 1681 RBL 50 WEB, ORIGINAL THICKNESS MAT OF WEB.071", MAT REM.054", MAT LOSS.017" FOUND OUT OF LIMTS IAW SRM 53-60-15
- [SDR FDEA201906271419](https://openairdocs.org/sdr/FDEA201906271419.md): Battery Pack · inoperative · Jun 27, 2019 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ABOVE R1 DOOR AND COCKPIT DOOR INOP. REMOVED AND REPLACED NR 1 RADIANT POWER CORP BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.
- [SDR FDEA201810162935](https://openairdocs.org/sdr/FDEA201810162935.md): Light · inoperative · Oct 16, 2018 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > L1 DOOR EXTERIOR EMER EXIT LIGHT IS INOP. RELAMPED L1 EMER EXIT SLIDE LIGHT REF AMM 33-51-06-2-1, OP'S NORMAL. HISTORY SHOWS POWER SUPPLY R&R AND LOOSE GROUND WIRE RESECURED, RELAMPED AT THIS TIME OP'S AS ADVERTISED WHEN OPERATED BY EMER LIGHT TEST SWITCH ABO
- [SDR FDEA2018091412302](https://openairdocs.org/sdr/FDEA2018091412302.md): Ground Wire · loose · Aug 31, 2018 · N995FD · Boeing 7572Q8 · Light System Wiring
  > L1 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED LIGHT ASSY FROM A/C FOUND GROUND WIRE LOOSE TIGHTEN WIRE PER GMP AND OPS CHECKED SYSTEM. ALL LITES OK.
- [SDR FDEA201804261129](https://openairdocs.org/sdr/FDEA201804261129.md): Computer · malfunctioned · Apr 26, 2018 · N995FD · Boeing 7572Q8 · Air Collision Avoidance System
  > TCAS WAS NOT SHOWING MULTIPLE KNOWN OTHER TRAFFIC AND ON FINAL COURSE TRAFFIC DIRECTLY IN FRONT OF AIRCRAFT WAS DISPLAYED 20 TO 30 DEGREES RIGHT OF NOSE. REMOVED AND REPLACED THE TCAS COMPUTER IAW AMM 34-45-01-4-99, AND TESTED IAW AMM 34-45-00-5-99. ACFT
- [SDR FDEA201712013329](https://openairdocs.org/sdr/FDEA201712013329.md): Skin · mechanic error · Dec 1, 2017 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > REPAIR DOUBLER AT STA. 1380-1400 S23L-26L DOES NOT COMPLY WITH THE SRM. ALL WORK WAS ACCOMPLISHED IAW FEDEX EA F-5330-T0336912 P1 FUSELAGE - PLATES & SKINS - FUSELAGE SKIN REPAIR BETWEEN STA 1380 AND 1400 BETWEEN STRINGERS S-23L AND S-26L
- [SDR FDEA201712013328](https://openairdocs.org/sdr/FDEA201712013328.md): Skin · mechanic error · Dec 1, 2017 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > REPAIR DOUBLER AT STA. 1380-1400 S20L-22L DOES NOT COMPLY WITH THE SRM. ALL WORK WAS ACCOMPLISHED IAW FEDEX EA F-5330-T0336913 P1 FUSELAGE- PLATES & SKINS - FUSELAGE SKIN REPAIR BETWEEN STA 1380 AND STA 1400 BETWEEN STRINGERS S-20L AND S-22L
- [SDR FDEA201712013327](https://openairdocs.org/sdr/FDEA201712013327.md): Skin · mechanic error · Dec 1, 2017 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > REPAIR DOUBLER AT STA. 1560-1580 S17R TO 20R DOES NOT COMPLY WITH THE SRM. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5330-T0336798 P1 FUSELAGE PLATES & SKINS - FUSELAGE SKIN REPAIR BETWEEN STA. 1560 AND 1580 BETWEEN STRINGERS S-17R AND S20R
- [SDR FDEA201711283318](https://openairdocs.org/sdr/FDEA201711283318.md): Floorbeam · corroded · Nov 28, 2017 · N995FD · Boeing 7572Q8 · Fuselage Main, Floor Beam
  > FORWARD WET AREA CORROSION STA 345 FLOORBEAM UPPER CHORD UPPER SURFACE, APPROX BBL 0- LBL 25. REMOVED CORR. ON FLOOR BEAM UPPER CHORD IAW B757 SRM 51-10-02 @ STA 345 100% MAT LOSS. REPAIRED UPPER T-CHORD IAW B757 SRM 53-00-51-2R REP 3
- [SDR FDEA201711283317](https://openairdocs.org/sdr/FDEA201711283317.md): Seat Track · corroded · Nov 28, 2017 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD WET AREA CORROSION LBL8 SEAT TACK FORWARD FLANGE, UPPER SURFACE AT NUT PLATE RIVETS APPROX STA 370. REMOVED CORR LBL8 APPROX STA. 370 SEAT TRACK IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS IAW B757 SRM 53-00-52. REMOVED SEAT TRACK IAW B
- [SDR FDEA201711283316](https://openairdocs.org/sdr/FDEA201711283316.md): Floorbeam · corroded · Nov 28, 2017 · N995FD · Boeing 7572Q8 · Fuselage Main, Floor Beam
  > FORWARD WET AREA CORROSION UPPER CHORD, UPPER SURFACE OF STA 365 FLOORBEAM, APPROX RBL 50. REMOVED PREVIOUS REPAIR ON FLOOR BEAM @ STA 365 DUE TO NO ALLOWABLE DAMAGE. REPAIRED UPPER T-CHORD STA 365 IAW B757 SRM 53-00-51-2R REPAIR 3
- [SDR FDEA201710172967](https://openairdocs.org/sdr/FDEA201710172967.md): Power Supply · inoperative · Oct 17, 2017 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > L1 DOOR EMERGENCY SIGN AND L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2, ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS CHECKED NORMAL.
- [SDR FDEA201701100110](https://openairdocs.org/sdr/FDEA201701100110.md): Light · inoperative · Jan 10, 2017 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > RT EXTERIOR SLIDE LIGHT IS INOP. RELEASED FOR SERVICE PER MEL 33-51-02-02.
- [SDR FDEA201511273800](https://openairdocs.org/sdr/FDEA201511273800.md): Panel · corroded · Nov 27, 2015 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT 9G SHEAR WEB AT STATION 422.5, RBL 15.5, AREA CORROSION. COMPLIED WITH EA F-5310-T0321795 PT1 FUSELAGE-MAINFRAME-MAIN CABIN SHEAR PANEL CORROSION REPAIR AT STA 422 BETWEEN BL0 AND RBL 24.
- [SDR FDEA201508052470](https://openairdocs.org/sdr/FDEA201508052470.md): Door Sill · dirty · Aug 5, 2015 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous Structure
  > L1 CABIN DOOR HANDLE EXTREMELY HARD TO ROTATE & LOCKED CLOSED. CLEANED DEBRIS FROM L1 DOOR SILL & GIRT BAR FLOOR FITTINGS. L1 DOOR OPERATIONS CHECKED NORMAL. OK FOR SERVICE. REFERENCE MM 52-11-00-0.
- [SDR FDEA201506292115](https://openairdocs.org/sdr/FDEA201506292115.md): Light · inoperative · Jun 29, 2015 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > ONE EXT EMER LIGHT INOPERATIVE. RELAMPED IAW SMP, OPERATIONS NORMAL IAW AMM 33-51-00-5.
- [SDR FDEA201404050667](https://openairdocs.org/sdr/FDEA201404050667.md): Cam · worn · Apr 5, 2014 · N995FD · Boeing 7572Q8 · Passenger/Crew Doors
  > L1 DOOR IS JAMMED. R & R L1 DOOR CONTROL CAM & FWD CRANK BEARING, OPERATIONS CHECKED GOOD IAW AMM 52-11-13-2 & IPC 52-11-13-01C.
- [SDR FDEA201311142784](https://openairdocs.org/sdr/FDEA201311142784.md): Skin · punctured · Nov 14, 2013 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
  > ACFT SKIN PUNCTURED BS 1622 BETWEEN S25-26R. REMOVED DAMAGE IAW SRM 51-10-02. FABRICATED REPAIR DOUBLER, STRINGER FILLER AND FILLER IAW SRM 51-40-05, 51-40-08, EA F-5330-T0304035 PT 1. INSTALLED REPAIR DOUBLER, STRINGER FILLER, FILLER IAW EA F-5330- T0304
- [SDR FDEA201301260195](https://openairdocs.org/sdr/FDEA201301260195.md): Lamp · inoperative · Jan 26, 2013 · N995FD · Boeing 7572Q8 · Emergency Lighting
  > L1 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-2-1.
- [SDR FDEA201212254374](https://openairdocs.org/sdr/FDEA201212254374.md): Cover · dislodged · Dec 25, 2012 · N995FD · Boeing 7572Q8 · Fuselage, Door Hinge
  > WHILE OPENING L1 CREW ENTRY DOOR UPPER DOOR HINGE COVER FELL OFF. REPLACED L1 DOOR UPPER HINGE PLATE IN REF TO SRM 51-40-02.
- [SDR FDEA201212064252](https://openairdocs.org/sdr/FDEA201212064252.md): Windshield · failed · Dec 6, 2012 · N995FD · Boeing 7572Q8 · Flight Compartment Windows
  > F/O'S WINDSCREEN SHATTERED ON CLIMBOUT AFTER DE-ICING. RETURNED TO DEPARTURE IAW QRH. R & R IAW AMM 56-11-01-4. F/O'S WINDOW CHECKED SERVICEABLE.
- [SDR FDEA201208042855](https://openairdocs.org/sdr/FDEA201208042855.md): Cam · out of rig · Aug 4, 2012 · N995FD · Boeing 7572Q8 · Passenger/Crew Doors
  > DURING B CHECK, L1 DOOR UPPER FWD CAM PLATE NEEDS TO BE RIGGED. ACCOMPLISHED RIGGING OF L1 DOOR UPPER FWD CAM PLATE IAW AMM. NO FAULTS NOTED.
- [SDR FDEA201208042854](https://openairdocs.org/sdr/FDEA201208042854.md): Roller · out of adjust · Aug 4, 2012 · N995FD · Boeing 7572Q8 · Passenger/Crew Doors
  > DURING B-CHECK, FOUND L1 DOOR UPPER FWD CRANK ARM ROLLER CONTACTS THE CAM PLATE WHEN CLOSING THE DOOR. ACCOMPLISHED RIGGING OF L1 DOOR UPPER FWD CRANK ROLLER CAM PLATE AND ROLLER IAW AMM NO FAULTS NOTED.
- [SDR FDEA201207312768](https://openairdocs.org/sdr/FDEA201207312768.md): Circuit Breaker · malfunctioned · Jul 31, 2012 · N995FD · Boeing 757236 · Emergency Lighting
  > RT SIDE EMERGENCY EXIT LIGHT STAYS ILLUMINATED WITH DOOR ARMED AND DISARMED. RESET CIRCUIT BREAKERS AND PERFORMED OPS CHECK IAW MM 33-51-00-5. OPS CHECKED GOOD.
- [SDR FDEA201207262701](https://openairdocs.org/sdr/FDEA201207262701.md): Window · out of adjust · Jul 26, 2012 · N995FD · Boeing 7572Q8 · Flight Compartment Windows
  > CAPTAIN`S SLIDING WINDOW DOES NOT STAY CLOSED WITH LATCH LOCKED CLOSED. WINDOW WILL CRANK OPEN WITH WINDOW LOCKED CLOSED. PERFORMED ADJUSTMENT TEST IAW MM 56-11-02-5. CAPTAINS SLIDING WINDOW, OPS CHECK NORMAL. RII ACCOMPLISHED.
- [SDR FDEA201207262700](https://openairdocs.org/sdr/FDEA201207262700.md): Window · out of adjust · Jul 26, 2012 · N995FD · Boeing 7572Q8 · Flight Compartment Windows
  > F/O SLIDING WINDOW DOES NOT STAY CLOSED WITH LOCK IN LOCKED CLOSED. WINDOW WILL CRANK OPEN WITH WINDOW IN LOCKED CLOSED. PERFORMED ADJUSTMENT TEST OF F/O'S SLIDING WINDOW IAW MM 56-11-02-5. FINAL CLOSED.

Next page: https://openairdocs.org/aircraft/N995FD/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 = 'N995FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N995FD/reports

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