# Service difficulty reports: N961FD

A list on [N961FD](https://openairdocs.org/aircraft/N961FD.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 · 80 reports

- [SDR FDEA202403070260](https://openairdocs.org/sdr/FDEA202403070260.md): Reservoir · low pressure · Mar 7, 2024 · N961FD · Boeing 7572Y0 · Emergency Equipment
  > L1 DOOR EMERGENCY POWER RESERVOIR NEEDS SERVICING. OUT OF GREEN BAND RANGE. INSPECTED L1 DOOR POWER RESERVOIR REF AMM 52-11-30-6-0. RESEVOIR PRESSURE GAUGE IS IN THE GREEN BAND. NO SERVICE NEEDED. R&R L1 DOOR SLIDE AS REQUESTED IAW AMM 25-66-01-4-0. OPS CH
- [SDR FDEA202310161769](https://openairdocs.org/sdr/FDEA202310161769.md): Gust Lock · damaged · Oct 16, 2023 · N961FD · Boeing 757200 · Passenger/Crew Doors
  > MDIS 961 52-10 9274 13OCT23 MEM FACT U L1 DOOR GUST LOCK BROKEN. MEL 13OCT23 06:26 MEM U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 16OCT23 "MEL 52-11-01-A: L1 DOOR - INOP." REMOVED BROKEN GUST LOCK PARTS TO ALLOW
- [SDR FDEA202301130089](https://openairdocs.org/sdr/FDEA202301130089.md): Relay · failed · Jan 13, 2023 · N961FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > ON APPROACH, TE LIGHT WITH TE FLAP DISAGREE MESSAGE, WHEN FLAPS SET TO 25. CONFIRMED FLAP HANDLE IN DETENT. COMPLIED WITH QRH FOR SUBSEQUENT APPROACH & LANDING. TROUBLESHOT IAW AMM 27-51 TREE 805, FSEU NR 1 SHOWED FLAP FAIL 217. DURING TEST OF FSEU 1, HAD F
- [SDR FDEA202209222356](https://openairdocs.org/sdr/FDEA202209222356.md): Fseu · failed · Sep 22, 2022 · N961FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > MOVING FLAP LEVER FROM 20 TO 25 A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE DISPLAYED. QRH COMPLIED WITH AND EMERGENCY DECLARED. EMERGENCY DECLARED. REMOVED AND REPLACED #1 FSEU IAW AMM 27-51-01-2. OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE.
- [SDR FDEA202206081394](https://openairdocs.org/sdr/FDEA202206081394.md): Gust Lock · damaged · Jun 8, 2022 · N961FD · Boeing 757200 · Passenger/Crew Doors
  > MDIS 961 52-10 8137 08JUN22 MEM OPEN U L1 DOOR GUST LOCK BROKEN MEL 08JUN22 05:17 MEM U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 11JUN22 "MEL 52-11-01-A: L1 DOOR INOP." C/7319881 PART 08JUN22 05:25
- [SDR FDEA202205101176](https://openairdocs.org/sdr/FDEA202205101176.md): Rod · sheared · May 10, 2022 · N961FD · Boeing 757200 · Nose/Tail Landing Gear
  > DURING TAXI-IN, NOTICED RIGHT NOSE GEAR DOOR, OPEN AND SWINGING. UPON BLOCK-IN, FOUND RIGHT NOSE GEAR ACTUATING ROD, REF IPC 32-22-02-01 FIG 1, ITEM 40, BROKEN OFF. REPLACED NOSE LANDING GEAR RH FWD DOOR OPERATING ROD IAW AMM 32-20-02-4 AND EA F-32
- [SDR FDEA202203090775](https://openairdocs.org/sdr/FDEA202203090775.md): None · none · Mar 9, 2022 · N961FD · Boeing 757200 · Emergency Lighting
  > EMERGENCY/ UNARMED LIGHT INOP RELAMPED THE EMERGENCY "UNARMED" ANNUNCIATION LIGHT OPS CK GOOD PER B 757 AMM 33-51-00-5. AC OK FOR SERVICE.
- [SDR FDEA202012233202](https://openairdocs.org/sdr/FDEA202012233202.md): Autopilot Sys · inoperative · Dec 23, 2020 · N961FD · Boeing 7572Y0 · Autopilot Computer
  > TEST FLIGHT: ON CLIMB OUT WITH CENTER AUTO PILOT ON, STAB TRIM WENT FULL UP. DISENGAGE AUTO PILOT AND WAS ABLE TO CONTROL TRIM. HAPPENED TWICE MORE ON CLIMBOUT. DURING DESCENT ON RT AUTOPILOT STAB TRIM WENT FULL NOSE DOWN TRIM. HAND FLOWN THE REMAINDER OF
- [SDR FDEA202012093089](https://openairdocs.org/sdr/FDEA202012093089.md): Floor Support · corroded · Dec 9, 2020 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > AFT CARGO INTERCOSTAL HAS CORROSION ON LOWER OUTBOARD SIDE AT RBL-5 STA 1417. REMOVED INTERCOSTAL AT AFT CARGO STA 1417 RBL 5 AND EVALUATED AND FOUND OUT OF LIMITS, IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00-04-1A FIG 101 DET V. REPLACED INTERCOSTAL BY FABR
- [SDR FDEA202012053044](https://openairdocs.org/sdr/FDEA202012053044.md): Cusp Web · corroded · Dec 5, 2020 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 580 AND STA 600. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA 580 TO STA 600 AND AFTER EVALUATION FOUND CUSP WEB OUT OF LIMITS, IAW B757 SRM 51-10-02, 53-30-13-1A FIG 101 DET VIII. FABRICATED AND INSTA
- [SDR FDEA202012053043](https://openairdocs.org/sdr/FDEA202012053043.md): Cusp Web · corroded · Dec 5, 2020 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 600 TO 620. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA. 600 TO 620 AND EVALUATED ORIGINAL MAT.036", MAT LOSS.015", MAT REM.021". FOUND OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. FABR
- [SDR FDEA202012053042](https://openairdocs.org/sdr/FDEA202012053042.md): Failsafe · corroded · Dec 5, 2020 · N961FD · Boeing 7572Y0 · Fuselage Main, Frame
  > MAIN CABIN LT SIDE JUST ABOVE STR 17 STA 1520 ON FRAME CORRODED. COMPLIED WITH FEDEX EA NR F-5310-T0358418 P1. FUSELAGE-MAINFRAME-STA 1520 FAILSAFE CHORD CORROSION ABOVE S-17L.
- [SDR FDEA202012043026](https://openairdocs.org/sdr/FDEA202012043026.md): Shim · cracked · Dec 4, 2020 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor Beam
  > MAIN CARGO FLOOR SUPPORT SHIM DAMAGED AT STA 1058 BETWEEN LBL 24 AND LBL 45. REMOVED SHIM (COVER PLATE) AT MAIN CARGO FLOOR SUPPORT STA 1058 BETWEEN LBL 24 AND LBL 45 AND FOUND CRACK AND OUT OF LIMITS, IAW B757 SRM 51-40-02-0G 53-00-51-1A. FABRICATED AND INS
- [SDR FDEA202012023015](https://openairdocs.org/sdr/FDEA202012023015.md): Seat Track · corroded · Dec 2, 2020 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL 45 STA 1540. REMOVED CORROSION AT MAIN CABIN SEAT TRACK FLANGE RBL 45 STA 1540 AND AFTER EVALUATION FOUND SEAT TRACK OUT OF LIMITS, IAW B757 SRM 51-10-02-0G AND B757 SRM 53-00-52-1A FIG 101 DET VII. REMOVED
- [SDR FDEA202012023014](https://openairdocs.org/sdr/FDEA202012023014.md): Seat Track · corroded · Dec 2, 2020 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABAIN STA 1540 LBL 45 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT MAIN CABIN STA 1540 LBL 45 SEAT TRACK FLANGE AND AFTER EVALUATION FOUND SEAT TRACK FLANGE OUT OF LIMITS, IAW B757 SRM 51-10-02-0G AND B757 SRM 53-00-52-1A FIG 101 DET VII. REMOVED A
- [SDR FDEA202012023013](https://openairdocs.org/sdr/FDEA202012023013.md): Crease Beam · corroded · Dec 2, 2020 · N961FD · Boeing 7572Y0 · Fuselage Main, Structure
  > MAIN CABIN RT SIDE STA 450 TO 665 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN RT SIDE CREASE BEAM BETWEEN STA 450 TO 665 AND AFTER EVALUATION FOUND CREASE BEAM OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101 DET VIII, SRM 51-10-02. REMOVED AND RE
- [SDR FDEA202009192256](https://openairdocs.org/sdr/FDEA202009192256.md): Compressor · stalled · Sep 19, 2020 · N961FD · Boeing 7572Y0 · Turbine Engine Compressor Section
  > PDIS 961 71-00 6706 19SEP20 ONT OPEN U LOGPAGES:3339293 AFTER TAKEOFF, AFTER SELECTING VNAV/CLIMB POWER, RIGHT ENGINE EXPERIENCED STRONG COMPRESSOR STALLS WITH LOUD CHUGS, LOSS OF POWER, AND HIGH EGT (905) COMPRESSOR STALL STOPPED WHEN THRU
- [SDR FDEA20200731732](https://openairdocs.org/sdr/FDEA20200731732.md): Handle · lack of lube · Jul 30, 2020 · N961FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE ON BASE TURN TO FINAL, WHEN GOING FROM FLAPS 20 TO 25. NO HISTORY PAST 90 DAYS. AFTER DEBREIFING CREW NO 'TE DISAGREE LIGHT' OR EICAS MESSAGE PRESENT. FSEU 1 SHOWED FLA FAIL. RESET FLAP ALTN SWITCH AND ROTARY SWITCH TO NORMAL AND RAN F
- [SDR FDEA202007211599](https://openairdocs.org/sdr/FDEA202007211599.md): Cover · loose · Jul 21, 2020 · N961FD · Boeing 7572Y0 · Escape Slide
  > SLIDE COVER ON L1 DOOR IS LOOSE. REPLACED DAMAGE POTED INSERTS ON UPPER HINGE COVER PANEL IAW AMM 25-00-00-8. INSTALLED SERVICEABLE SLIDE COVER IAW AMM 25-66-01-4.
- [SDR FDEA2020030970502](https://openairdocs.org/sdr/FDEA2020030970502.md): Unknown · odor · Mar 7, 2020 · N961FD · Boeing 7572Y0 · Air Distribution System
  > FUMES IN COCKPIT ON TAKEOFF ROLL TILL ABOUT 5K FT. REQUIRED CREW TO DON O2 MASK IMMEDIATELY AFTER TAKEOFF. ODOR OF BURNT RUBBER/ENG SMELL MAINLY ON CAPTAINS SIDE. FO DID NOT DETECT ODOR. ODOR CLEARED BEFORE CREW COULD SECURE ANY EQUIPMENT. NO FURTHER OCC
- [SDR FDEA201812053433](https://openairdocs.org/sdr/FDEA201812053433.md): Actuator · failed · Dec 5, 2018 · N961FD · Boeing 757200 · Leading Edge Slat Actuator
  > PDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGENCY DECLARED. COMPLETED INSTALLATION OF BAD ROTARY ACTUATORS IAW
- [SDR FDEA2018120653433](https://openairdocs.org/sdr/FDEA2018120653433.md): Actuator · failed · Dec 5, 2018 · N961FD · Boeing 7572Y0 · Leading Edge Slat Actuator
  > PDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGENCY DECLARED. COMPLETED INSTALLATION OF BAD ROTARY ACTUATORS IAW
- [SDR FDEA201811173272](https://openairdocs.org/sdr/FDEA201811173272.md): Stringer · cracked · Nov 17, 2018 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/Stringer
  > MAIN CABIN STA 1505 STR 1 CRACKED. REMOVED DAMAGED SECTION DIM 12" STA 1500 IAW SRM 53-00-03-2R REPAIR 2 FIG 201 DET 1. REMOVED FWD SECTION ON STR 1 FROM STA 1492 TO EXISTING SPLICED STA 1460 IAW SRM 51-40-02-0G. FABRICATED NEW REPAIR STRINGER SECTION AND SPLI
- [SDR FDEA201711223298](https://openairdocs.org/sdr/FDEA201711223298.md): Bottle · discharged · Nov 22, 2017 · N961FD · Boeing 7572Y0 · Passenger/Crew Doors
  > NR 1 PASSENGER DOOR ASSIST BOTTLE DISCHARGED, REQUIRES SERVICING. REMOVED AND REPLACED CYLINDER EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.
- [SDR FDEA201709162581](https://openairdocs.org/sdr/FDEA201709162581.md): Fseu · malfunctioned · Sep 16, 2017 · N961FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP DISAGREE LIGHT. LOCKED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FSEU BITE PROCEDURE IAW FIM 27-51-00, FIG 104, FOUND NO CURENT FAULTS FOR NR 1 FSEU FOUND FLA FAILDED ON SEVERAL TRIES COULD NOT GET A GOOD BITE ON NR 2 FSEU. REMOVED AN
- [SDR FDEA201708032108](https://openairdocs.org/sdr/FDEA201708032108.md): Seat Track · damaged · Aug 3, 2017 · N961FD · Boeing 7572Y0 · Cargo Compartments
  > LOCK ON CENTERLINE BETWEEN STRINGERS 3L-R FOUND DAMAGED AT SEAT TRACK. REMOVED LOCK AND PLACED IN COURRIER COMPT. LOCK ID D611 MEL 29JUN17 18:59 SEAT TRACK LOBE DAMAGED. WILL REQUIRE SHEET METAL FOR REPAIR. FOUND TRACK TO BE DAMAGED, APPROX 72 HOUR F
- [SDR FDEA201703290998](https://openairdocs.org/sdr/FDEA201703290998.md): Transmitter · malfunctioned · Mar 29, 2017 · N961FD · Boeing 7572Y0 · Leading Edge Slat Control System
  > AFTER TAKEOFF RECEIVED A LE SLAT DISAGREE EICAS. PERFORMED QRH. COMPLIED WITH LANDING PROCEDURES. REMOVED AND REPLACED LEADING EDGE PDU TRANSMITTER.
- [SDR FDEA201703291000](https://openairdocs.org/sdr/FDEA201703291000.md): Fuel Sys · leaking · Mar 29, 2017 · N961FD · Boeing 7572Y0 · Aircraft Fuel System
  > LEFT WING INBOARD DRY BAY CENTER FORWARD DRAIN HAS A RUNNING FUEL LEAK.
- [SDR FDEA201703240986](https://openairdocs.org/sdr/FDEA201703240986.md): Warning Message · false activation · Mar 24, 2017 · N961FD · Boeing 7572Y0 · Leading Edge Slat Control System
  > LE SLAT DISAGREE EICAS MESSAGE AS FLAP EXTENDED TO FLAPS 1, WENT THROUGH QRH PROCEDURE WHICH LEAD TO A LE SLAT ASSYMETRY ISSUE. PERFORMED QRH PROCEDURE FOR LE SLAT ASSYMETRY. NO NOTED ADVERSE ROLL OR YAW. NO AIRCRAFT LIMITS EXCEEDED. NO STATUS MESSAGES
- [SDR FDEA201703010723](https://openairdocs.org/sdr/FDEA201703010723.md): Connector · unsecure · Mar 1, 2017 · N961FD · Boeing 7572Y0 · Hydraulic Power System Wiring
  > DURING CRUISE FLIGHT AT FL390, A RAT UNLOCKED EICAS MESSAGE AND RAT UNLOCKED LIGHT IN RAT SWITCH ILLUMINATED. FIVE MINUTES LATER BOTH WARNINGS WERE NO LONGER DISPLAYED. NO RAT UNLOCKED MESSAGE AT BLOCK IN. DEPLOYED RAT IAW AMM 29-21-00-2 AND RECEIVED A R
- [SDR FDEA201610273707](https://openairdocs.org/sdr/FDEA201610273707.md): Skin · delaminated · Oct 27, 2016 · N961FD · Boeing 7572Y0 · Trailing Edge Flaps
  > RIGHT WING OB FLAP TOP SECTON INBD SIDE REPAIR DISBONED. REPAIRED IAW SRM 57-53-01-2R FIG 201, SRM 51-70-10 REPAIR 4, AND SRM 51-70-10-2R PARA 20, FIG 208.
- [SDR FDEA201610273714](https://openairdocs.org/sdr/FDEA201610273714.md): Door Frame · cracked · Oct 27, 2016 · N961FD · Boeing 7572Y0 · Passenger/Crew Doors
  > R2 DOOR UPPER HINGE CUTOUT IS CRACKED. LOCATED AND INSTALLED REPAIR DOUBLER PN 143N6158-12 AT R2 DOOR UPPER HINGE CUT OUT IAW SRM 52-10-02-2R. COMPLIED WITH EA F-5210-T0329362 P1. MAJOR REPAIR.
- [SDR FDEA201507312445](https://openairdocs.org/sdr/FDEA201507312445.md): Door · delaminated · Jul 31, 2015 · N961FD · Boeing 7572Y0 · Landing Gear Doors
  > LEFT MLG DOOR DELAMINATED. MISSING SECTION CRAZ COMPLY WITH EA F-5280-T0319221 REV NR POS P3. R & R MLG DOOR IAW MM 32-12-01-4 & EA F-5280-T0319221.
- [SDR FDEA201507192271](https://openairdocs.org/sdr/FDEA201507192271.md): Bracket · loose · Jul 19, 2015 · N961FD · Boeing 7572Y0 · Escape Slide
  > L1 DOOR SLIDE COVER LOOSE. TIGHTENED SLIDE COVER ATTACH BRACKETS, AND INSTALLED SLIDE COVER FOR L1 DOOR IAW AMM 52-11-02-4.
- [SDR FDEA201505201570](https://openairdocs.org/sdr/FDEA201505201570.md): Brake · lack of lube · May 20, 2015 · N961FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > RECEIVED TE FLAP DISAGREE EICAS MSG ON APPROACH WHEN MOVING FLAPS FROM 20' TO 25'. RETRACTED FLAP HANDLE TO 20' IAW GO AROUND PROCEDURES, RAN QRH & LANDED FLAPS 20' TROUBLE SHOT FLAP DISAGREE IAW FIM 27-51 FAULT TREE 808. FOUND LT OTBD FLAP TRANSMISSION OVER
- [SDR FDEA201411253894](https://openairdocs.org/sdr/FDEA201411253894.md): Skin · dented · Nov 25, 2014 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > FUSELAGE HAS A DENT AT BS 525 BETWEEN STRINGERS 26 - 27L. REPAIRED IAW EA F-5330-T0313598 REV P1. MAJOR REPAIR.
- [SDR FDEA201407091672](https://openairdocs.org/sdr/FDEA201407091672.md): Light · inoperative · Jul 9, 2014 · N961FD · Boeing 7572Y0 · Emergency Lighting
  > DURING PREFLIGHT CHECK, FOUND R1 DOOR EMER SLIDE LIGHT INOPERATIVE. RELAMPED R1 DOOR SLIDE LIGHT, OPERATIONS CHECKED NORMAL.
- [SDR FDEA201407091671](https://openairdocs.org/sdr/FDEA201407091671.md): Pin · backed out · Jul 9, 2014 · N961FD · Boeing 7572Y0 · Light System Wiring
  > DURING PREFLIGHT, FOUND L1 DOOR EMER SLIDE LIGHT INOPERATIVE. REMOVED LIGHT ASSEMBLY & CHECKED VOLTAGE TO LIGHT WITH EMER LIGHTS ON, THERE IS NO POWER TO L1 SLIDE LIGHT. DURING TROUBLESHOOTING FOUND PIN 9 OF PLUG D68 PUSHED BACK INTO PLUG BATTERY CHARGER CON
- [SDR FDEA201302250457](https://openairdocs.org/sdr/FDEA201302250457.md): Battery · inoperative · Feb 25, 2013 · N961FD · Boeing 7572Y0 · Emergency Lighting
  > DOOR EMERGENCY EXIT LIGHTS WILL NOT TEST. R & R L1 EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.
- [SDR FDEA201212104273](https://openairdocs.org/sdr/FDEA201212104273.md): Web · damaged · Dec 10, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > MAIN DECK- CARGO DOOR CUTOUT ON FUSELAGE SILL AREA LOWER SILL WEB HAS A PUNCTURE LOCATED JUST AFT OF NR 1 DOOR LATCH FITTING. A REPAIR WAS ACCOMPLISHED ON THE LOWER DOOR SILL WEB BY EA 757-5331-16-F4054. MAJOR REPAIR.
- [SDR FDEA201212054250](https://openairdocs.org/sdr/FDEA201212054250.md): Track · failed · Dec 5, 2012 · N961FD · Boeing 7572Y0 · Cargo Compartments
  > THE CARGO HANDLING SYS, ROLLER RAILS WILL NOT LOCK INTO THE SEAT TRACK CROWNS BETWEEN STA, S660-780 RBL 24.75 AND 45.5. DISCEPANT SEAT TRACKS ARE INCOMING. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD, A REPAIR WAS PERFORMED ON STAM EA 757-5335-16-F4048
- [SDR FDEA201212044245](https://openairdocs.org/sdr/FDEA201212044245.md): Skin · corroded · Dec 4, 2012 · N961FD · Boeing 7572Y0 · Trailing Edge Flaps
  > LT INBD FLAP, FRONT INBD PANEL HAS CORROSION. REMOVED CORROSION ON LT INBD FLAP INBD PANEL IAW-SRM-51-10-02. CHECK LIMIT ORIG MAT.125 MAT LOSS.030 FOUND OUT OF LIMIT IAW-SRM-57-53-01, FIG 101, DET VIII PG 106, WORK ACCOMPLISHED ON EA F-5750-162474. CAT "A
- [SDR FDEA201211214119](https://openairdocs.org/sdr/FDEA201211214119.md): Stringer Clip · corroded · Nov 21, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Attach Fittings
  > FOUND CORROSION AT BS 1661 S26R STINGER CLIP. REPAIRED IAW SRM 53-00-03 REPAIR 2.
- [SDR FDEA201211144019](https://openairdocs.org/sdr/FDEA201211144019.md): Skin · dented · Nov 14, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE AT BS 380 STRINGER 4R A FUSELAGE EXTERNAL SKIN REPAIR WAS ACCOMPLISHED BETWEEN STA 377-418 IAW EA 757-5311-16-F3939 REV-. MAJOR REPAIR.
- [SDR FDEA201211093928](https://openairdocs.org/sdr/FDEA201211093928.md): Skin · dented · Nov 9, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > SKIN DENTED BS 1630 BETWEEN S17 TO 18R. DENT REPAIRED IAW EA 757-5361-16-F3919. MAJOR REPAIR.
- [SDR FDEA201211093926](https://openairdocs.org/sdr/FDEA201211093926.md): Skin · misrepaired · Nov 9, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN MISREPAIRED BS 395 BETWEEN S1 TO 3L. REPAIRED IAW EA 757-5311-16-F3891, REV-.
- [SDR FDEA201211083914](https://openairdocs.org/sdr/FDEA201211083914.md): Stringer · corroded · Nov 8, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/Stringer
  > STRINGER 17R BS 1420-1440 CORRODED REPAIRED EA 757-5361-16-F3901. MAJOR REPAIR.
- [SDR FDEA201211073904](https://openairdocs.org/sdr/FDEA201211073904.md): Panel · corroded · Nov 7, 2012 · N961FD · Boeing 7572Y0 · Leading Edge Devices
  > NR 2 SLAT COVE PANEL JUST BELOW INBD MAIN TRACK FITTING HAS CORROSION. REMOVED CORROSION ON COVE PANEL IAW SRM 51-10-02. REMOVED.019 FROM ORIGINAL THICKNESS OF.050 AND.031 WAS REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DETAIL III, V
- [SDR FDEA201211023813](https://openairdocs.org/sdr/FDEA201211023813.md): Structure · misrepaired · Nov 2, 2012 · N961FD · Boeing 7572Y0 · Cargo/Baggage Doors
  > CARGO DOOR LWR FWD CORNER MISREPAIRED. REPAIRED IAW-SRM-52-30-01 FIG.201 REPAIR 4 THIS IS A CAT."B" REPAIR,MAJOR.
- [SDR FDEA201211013808](https://openairdocs.org/sdr/FDEA201211013808.md): Skin · damaged · Nov 1, 2012 · N961FD · Boeing 7572Y0 · Wing, Plate/Skin
  > LEFT WING TOP OTBD WINGTIP HAS A LIGHTING STRIKE. FOUND LIGHTENING STRIKE TO BE ON SCREW AND SPLICE STRAP. REMOVED AND REPLACED OUTBOARD RIB LT WING SPLICE STRAP AND SCREW IAW SRM 51-40-02 AND DWG 112N5027. MAJOR REPAIR

Next page: https://openairdocs.org/aircraft/N961FD/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 = 'N961FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N961FD/reports

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