# Service difficulty reports: N971FD

A list on [N971FD](https://openairdocs.org/aircraft/N971FD.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 · 116 reports

- [SDR FDEA202307181240](https://openairdocs.org/sdr/FDEA202307181240.md): Lamp · failed · Jul 18, 2023 · N971FD · Boeing 757200 · Emergency Lighting
  > MDIS 971 33-50 9241 18JUL23 BMI FACT U R1 DOOR EXTERIOR SLIDE LIGHT INOP FACT 18JUL23 15:12 BMI U AMM: 33-51-06-2-1 REMOVED AND REPLACED R1 DOOR EXT SLIDE LIGHT BULB MPN 767 NSN CHECKED GOOD PER REF B757 AMM 33-51-06-2-1 AMM: 33-51-06-2-
- [SDR FDEA202302280353](https://openairdocs.org/sdr/FDEA202302280353.md): Fitting · cracked · Feb 28, 2023 · N971FD · Boeing 757200 · Wing, Plate/Skin
  > WHILE PERFORMING OPEN HOLE HFEC INSP OF RH WING UPPER SKIN AND DRAG FITTING FOUND HOLE #3 TO HAVE A CRACK INDICATION AT APPROX O'CLOCK FACING FWD. REMVOED RH IB DRAG FITTING, REPAIR UPPER WING SKIN, INSTALLED NEW FITTING IAW EA # F- 5730-T0372720 P1.
- [SDR FDEA202302280352](https://openairdocs.org/sdr/FDEA202302280352.md): Fitting · cracked · Feb 28, 2023 · N971FD · Boeing 757200 · Wing, Plate/Skin
  > WHILE ACCOMPLISHING OPEN HFEC OF LH WING UPPER SKIN AND AROUND DRAG FITTING FOUND HOLE #18 TO HAVE A CRACK INDICATION AT APPROX. 1 O'CLOCK FACING FWD. REMOVED LH OB DRAG FITTING, REPAIR FITTINGS AND UPPER WING SKIN AND REINSTALLED FITTING IAW EA# F-5730-T0
- [SDR FDEA202302280351](https://openairdocs.org/sdr/FDEA202302280351.md): Fitting · cracked · Feb 28, 2023 · N971FD · Boeing 757200 · Wing, Plate/Skin
  > WHILE PERFORMING OPEN HOLE HFEC INSP FO RH WING UPPER SKIN AND DRAG FITTING FOUND HOLE #5 TO HAVE CRACK INDICATIONS AT APPROX 7 O'CLOCK. REMOVED RH OB DRAG FITTING, REPAIR UPPER WING SKIN, INSTALLED NEW FITTING IAW EA# F- 5730-T0372720 P1.
- [SDR FDEA202302280350](https://openairdocs.org/sdr/FDEA202302280350.md): Fitting · cracked · Feb 28, 2023 · N971FD · Boeing 757200 · Wing, Plate/Skin
  > WHILE ACCOMPLISHING OPEN HOLE HFEC INSP OF LH WING UPPER SKIN AND DRAG FITTING FOUND HOLE #3 TO HAVE A CRACK INDICATION AT APPROX 3 O'CLOCK FACING FWD. REMOVED LH IB DRAG FITTING, REPAIRED UPPER SKIN AND INSTALLED NEW FITTING IAW EA# F- 5730-T0372758 P1.
- [SDR FDEA202211162798](https://openairdocs.org/sdr/FDEA202211162798.md): Actuator · failed · Nov 16, 2022 · N971FD · Boeing 75728A · Leading Edge Slat Control System
  > SELECTED FLAPS 1 AT 5500 FEET AND ABOUT 200 KNOTS. RECEIVED LE SLAT DISAGREE EICAS MESSAGE. COMPLIED WITH QRH. MESSAGE REMAINED. QRH DIRECTED US TO RUN LE SLAT ASYMMETRY QRH. COMPLIED WITH QRH. DECLARED EMERGENCY AND LANDED WITH TE FLAPS AT 20 WITH NO FURTHER
- [SDR FDEA202208121974](https://openairdocs.org/sdr/FDEA202208121974.md): Idg · failed · Aug 12, 2022 · N971FD · Boeing 757200 · AC Generator-Alternator
  > DURING CLIMB OUT AT 600 FEET L GEN OFF ILLUMINATED. RAN QRH AND ABLE TO RESET L GEN. STARTED APU FOR BACKUP AND APU RAN FOR ABOUT 5 MINUTES AND GOT AN APU FAULT EICAS AND APU SHUTDOWN. DURING DESCENT L GEN OFF EICAS ILLUMINATED AGAIN. QRH ONLY ALLOWS ONE
- [SDR FDEA202104271051](https://openairdocs.org/sdr/FDEA202104271051.md): Fseu · failed · Apr 27, 2021 · N971FD · Boeing 75728A · Trailing Edge Flap Control System
  > ON ILS 11 KPWM GOT LE SLAT DISAG AUDIBLE WARNING, BUT NO EICAS MESSAGE DISPLAYED. WHEN FLAPS POSITIONED TO FLAPS 15 THEN RECEIVED EICAS MESSAGE LE SLAT DISAG. NO SPLIT FLAP NEEDLES ON FLAP INDICATOR. FLAPS STOPPED MOVEMENT HYDRAULICALLY AT FLAPS 1. COMPL
- [SDR FDEA202102120344](https://openairdocs.org/sdr/FDEA202102120344.md): Sensor · binding · Feb 12, 2021 · N971FD · Boeing 75728A · Door Warning System
  > R1 DOOR LEVER PHYSICALLY MOVED ABOVE THE PANEL THAT COMES OUT WHEN THE DOOR IS CLOSED, UPON LANDING BLOCK IN MESSAGE/SUMMARY CAME UP BEFORE LEAVING THE RUNWAY. FAULT SEEMS TO OCCUR DURING CLIMBOUT AND PRESSURIZATION. RMVD SLIDE COVER AND INSPECTED FOR
- [SDR FDEA202101170142](https://openairdocs.org/sdr/FDEA202101170142.md): Floor Panel · delaminated · Jan 17, 2021 · N971FD · Boeing 75728A · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL 222BF DELAMINATED. FABRICATED MAIN CABIN FWD WET AREA FLOOR PANEL 222BF, IAW B757 AMM 53-01-01-7 AND FEDEX DWG SRZ-25-005.
- [SDR FDEA202101110051](https://openairdocs.org/sdr/FDEA202101110051.md): Panel · cracked · Jan 11, 2021 · N971FD · Boeing 75728A · Wing, Plate/Skin
  > RT WING NR 10 SLAT LOWER COVE PANEL HAS EVIDENCE OF CRACK ON OUTBOARD SIDE OF OUTBOARD MAIN TRACK. REPAIRED RT WING NR 10 SLAT LOWER COVE PANEL ON OUTBOARD SIDE OF OUTBOARD MAIN TRACK, IAW B757 SRM 57-43-01-2R REP 4.
- [SDR FDEA202101110050](https://openairdocs.org/sdr/FDEA202101110050.md): Panel · cracked · Jan 11, 2021 · N971FD · Boeing 75728A · Wing, Plate/Skin
  > RT WING NR 10 SLAT LOWER COVE PANEL HAS EVIDENCE OF CRACK ON INBOARD SIDE OF OUTBOARD MAIN TRACK. REPAIRED RT WING NR 10 SLAT LOWER COVE PANEL ON INBOARD SIDE OF OUTBOARD MAIN TRACK, IAW B757 SRM 57-43-01-2R REP 4.
- [SDR FDEA202101030002](https://openairdocs.org/sdr/FDEA202101030002.md): Floor Support · corroded · Jan 3, 2021 · N971FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR SUPPORT CHANNEL HAS CORROSION AT RBL-58 BETWEEN STA 324 AND STA 345. REMOVED CORROSION ON SUPPORT CHANNEL STA 324 AND STA 345 RBL 58, IAW B757 SRM 51-10-02. ORIG MAT.050 LOSS.040 REM.010 OUT OF LIMITS, IAW B757 SRM 5300-51-1A FIG 101. RE
- [SDR FDEA202101030006](https://openairdocs.org/sdr/FDEA202101030006.md): Web · corroded · Jan 3, 2021 · N971FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT WEB HAS MULTIPLE AREAS OF CORROSION AT LBL 58 BETWEEN STA 1635 AND STA 1681. REMOVED CORR ON WEB LBL 58 STA 1635-1681, IAW B757 SRM 51-10-02. ORIG MAT.056 REM.028 LOSS.028 FOUND OUT OF LIMITS, IAW B757 SRM 53-60-15-1A FIG 101. RE
- [SDR FDEA202101030004](https://openairdocs.org/sdr/FDEA202101030004.md): Crease Beam · corroded · Jan 3, 2021 · N971FD · Boeing 75728A · Fuselage Main, Structure
  > MAIN CABIN FLOOR CREASE BEAM STA 876 RT SIDE CORRODED. REMOVED CORROSION ON CREASE BEAM STA 876 RT SIDE, IAW B757 SRM 51-10-02. ORIG MAT.071 REM.046 LOSS.025 FOUND OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101. REPAIRED CREASE BEAM, IAW B757 SRM 53-00
- [SDR FDEA202012293217](https://openairdocs.org/sdr/FDEA202012293217.md): Panel · cracked · Dec 29, 2020 · N971FD · Boeing 75728A · Cargo/Baggage Doors
  > MAIN CARGO DOOR FWD PRESSURE DOOR INTERNAL DAMAGED (CRACK) AT THE WEB. REMOVED, FABRICATED AND INSTALLED NEW FWD PANEL (WEB) ON MAIN CARGO DOOR, IAW B757 SRM 51-40-02, 51-30-01, 51-40-05 AND BOEING DWG 65-49309 REV D. APPLIED CIC IAW FEDEX DWG B57-50-001 REV
- [SDR FDEA202012293218](https://openairdocs.org/sdr/FDEA202012293218.md): Panel · dented · Dec 29, 2020 · N971FD · Boeing 75728A · Cargo/Baggage Doors
  > MAIN CARGO DOOR AFT PRESSURE DOOR INTERNAL PROTRUDING DENTS AT THE WEB. REMOVED, FABRICATED, AND INSTALLED NEW AFT PANEL (WEB) ON MAIN CARGO, IAW B757 SRM 51-40-02 51-30-01, 51-40-05 AND BOEING DWG 65-49309 REV D. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS
- [SDR FDEA202012213193](https://openairdocs.org/sdr/FDEA202012213193.md): Seat Track · corroded · Dec 21, 2020 · N971FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS COORSION @ RBL-57 BETWEEN STA. 1180 AND STA. 1300 REMOVED CORR ON SEAT TRACK STA 1180-1300 RBL58 IAW B757 SRM 51-10-02 ORIG MAT.090 REM.057 LOSS.037 OUT OF LIMITS IAW BAC 1520-792 BOEING DWG. REPAIR SEAT TRACK IAW B757
- [SDR FDEA202003270609](https://openairdocs.org/sdr/FDEA202003270609.md): Warning System · false activation · Mar 27, 2020 · N971FD · Boeing 75728A · Elevator Control System
  > PDIS 971 27-30 6467 ON CLIMB IN CLEAR CONFIGURATION RECIVED EICAS MSG RUDDER RATIO AND MACH / SDD TRIM (AND OVERHEAD LT) ALONG WITH ELEV ASYM ON STATUS PAGE, NO AUTO PILOT, RAN QRH, NO HELP, CONTACTED GOC & COORDINATED RETURN TO SERVICE PERFORMED
- [SDR FDEA2019102422726](https://openairdocs.org/sdr/FDEA2019102422726.md): Cover · unsecure · Oct 22, 2019 · N971FD · Boeing 75728A · Escape Slide
  > NOTICED LEFT FORWARD ENTRYDOOR WAS BINDING. HAD MAINTENANCE OPEN DOOR FROM THE OUTSIDE. KMEM WHILE PERFORMING INSPECTION CHECK IN REF. TO AMM 52-11-01-6. FOUND COVER TO SLIDE NOT SECURE BINDING. RESECURED COVER IN REF. TO AMM 25-66-01-4. FOUND L1 DO
- [SDR FDEA201909122213](https://openairdocs.org/sdr/FDEA201909122213.md): Probe · obstructed · Sep 12, 2019 · N971FD · Boeing 75728A · Engine EGT/TIT Indicating System
  > PDIS 971 77-00 6015 12SEP19 RIC OPEN U LOGPAGES:3180701 CONTINUED FROM LOG PAGE 2966550, CONTINUED OPERATION OF RT ENG AT IDLE TO LANDING. FIRST INDICATION OF PROBLEM WAS 1 SEC AMBER EGT INDICATION ON RT ENG PRIOR TO THRUST REDUCTION. NO OTHER ACCOM
- [SDR FDEA2019081541866](https://openairdocs.org/sdr/FDEA2019081541866.md): Warning Message · false activation · Aug 14, 2019 · N971FD · Boeing 75728A · Drag Control System
  > ON TAKEOFF ROLL,WHEN ENGINES WERE SET TO TAKEOFF THRUST AND ABOUT 30 KNOT AIRSPEED RECEIVED A SPOILER EICAS WITH CORRESPONDING MASTER WARNING LIGHTS AND TONE. REJECTED TAKEOFF IAW QRH. UNABLE TO DUPLICATE THE ABOVE DISCREPENCY IAW FIM 27-61-00-815-802.
- [SDR FDEA201802220469](https://openairdocs.org/sdr/FDEA201802220469.md): Switch · failed · Feb 22, 2018 · N971FD · Boeing 75728A · Leading Edge Slat Control System
  > DURING FINAL APPROACH, RECEIVED A LEADING EDGE SLAT ASSYMETRY EICAS AND ASSOCIATED CUE LIGHT. RAN QRH PROCEDURES, FLAPS 20 LANDING. LANDING NORMAL. R & R THE RT LOSS SENSING SWITCH FOR THE L/E SLATS IAW MM 27-81-41-4. PREFORMED A TEST OF THE RT LOSS SENSING
- [SDR FDEA201711243302](https://openairdocs.org/sdr/FDEA201711243302.md): Seat Track · damaged · Nov 24, 2017 · N971FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > FOUND A BROKEN LOCK AT POS 3 MAIN DECK CENTER LINE. LOCK D611. FOUND DAMGED SEAT TRACK AT SAME LOCATION. COMPLIED WITH EA F-5320-T0336761 PART 1. REPAIRED THE SEAT TRACK BS 614 - 620, BL 0.
- [SDR FDEA201709062464](https://openairdocs.org/sdr/FDEA201709062464.md): Transmitter · out of adjust · Sep 6, 2017 · N971FD · Boeing 75728A · Trailing Flap Position Indicating System
  > RECEIVED EICAS MSG "TE FLAP ASYM" RAN QRH LANDED WITH MAX AUTO BRAKES LANDING WEIGHT 167.0LB. R&R LT TE FLAP POSITION XMITTER PER MM 27-58-03-4 AND PERFORM ADJ/TEST PER MM 27-58-01-5. TE FLAP INDICATION SYS OP'S CK. GOOD OK FOR SERVICE.
- [SDR FDEA201703280999](https://openairdocs.org/sdr/FDEA201703280999.md): Girt Bar · inoperative · Mar 28, 2017 · N971FD · Boeing 75728A · Emergency Equipment
  > R1 DOOR SLIDE ARM LIGHT WOULD NOT ARM. REMOVED AND REPLACED R1 GIRT BAR IAW MM 25-66-10-2. SLIDE ARM LIGHT OPS CHECKED GOOD. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201609143219](https://openairdocs.org/sdr/FDEA201609143219.md): Indicator · reads low · Sep 14, 2016 · N971FD · Boeing 75728A · Emergency Equipment
  > PRESSURE REGULATOR GAUGE ON R1 DOOR SHOWS RED. R & R THE R1 DOOR SLIDE IAW MM 25-66-01-4.
- [SDR FDEA201509303007](https://openairdocs.org/sdr/FDEA201509303007.md): Valve · leaking · Sep 30, 2015 · N971FD · Boeing 75728A · Hydraulic System, Main
  > LEFT HYD SYS LEAK & LOW FLUID FAILURE. SEVERAL ASSOCIATED EICAS & STATUS MSGS. LT HYD QTY WENT TO.12, FOLLOWED BY A LT QTY LOW EICAS MSG, LT RESERVOIR PSI LIGHT, SHUT PUMPS OFF UNTIL LANDING. ADDED 4 GALLONS TO LT HYD RESERVOIR, PRESSURIZED LT SYS, ISOLATE
- [SDR FDEA201509303006](https://openairdocs.org/sdr/FDEA201509303006.md): Bypass Valve · leaking · Sep 30, 2015 · N971FD · Boeing 75728A · Hydraulic System, Main
  > LEFT HYD SYS LEAK & LOW FLUID FAILURE. SEVERAL ASSOCIATED EICAS & STATUS MESSAGES. LT HYD QTY WENT TO.12, FOLLOWED BY A LT QTY LOW EICAS MESSAGE, LT RESERVOIR PSI LIGHT, SHUT PUMPS OFF UNTIL LANDING. EMERGENCY DECLARED, FOUND VALVE HYD PRESSURE REDUCER, RU
- [SDR FDEA201508232690](https://openairdocs.org/sdr/FDEA201508232690.md): Light · inoperative · Aug 23, 2015 · N971FD · Boeing 75728A · Emergency Lighting
  > R1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. RELAMPED R1 SLIDE LIGHT & CHECKED OK IAW AMM 33-51-06-2-1.
- [SDR FDEA201507022139](https://openairdocs.org/sdr/FDEA201507022139.md): Latch · loose · Jul 2, 2015 · N971FD · Boeing 75728A · Emergency Equipment
  > ESCAPE ROPE COVER ON CAPTAINS SIDE DOES NOT STAY LATCHED. BOTTOM LATCH LOOSE. SECURED BOTTOM LATCH ON CAPTAINS SIDE ESCAPE ROPE COVER & CLOSED PANEL.
- [SDR FDEA201412094087](https://openairdocs.org/sdr/FDEA201412094087.md): Panel · cracked · Dec 9, 2014 · N971FD · Boeing 75728A · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR AFT PRESS RELIEF DOOR COVE PANEL IS CRACKED.
- [SDR FDEA201412084080](https://openairdocs.org/sdr/FDEA201412084080.md): Shear Web · corroded · Dec 8, 2014 · N971FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MAIN DECK SHEAR WEB HAS CORROSION AT RBL 25 BS 420. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED & INSTALLED THE DOUBLER IAW SRM 51-40-02 & SRM 5 4 3.
- [SDR FDEA201412084079](https://openairdocs.org/sdr/FDEA201412084079.md): Shear Web · corroded · Dec 8, 2014 · N971FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MAIN DECK SHEAR WEB HAS CORROSION AT LBL 25 BS 420. REMOVED CORROSION, FABRICATED DOUBLER, LOCATED, DRILLED & INSTALLED THE DOUBLERIAW SRM 51-40-02 & SRM 5 4 3.
- [SDR FDEA201412044060](https://openairdocs.org/sdr/FDEA201412044060.md): Skin · cracked · Dec 4, 2014 · N971FD · Boeing 75728A · Cargo/Baggage Doors
  > MAIN CARGO DOOR INNER SKIN CRACKED. FABRICATED & INSTALLED NEW ACCESS PANEL ON MAIN CARGO DOOR INNER SKIN BS 500 - 520 IAW SRM 51-40-02 & DWG 65-49309 REV D.
- [SDR FDEA201404100710](https://openairdocs.org/sdr/FDEA201404100710.md): Fire Warning · false indication · Apr 10, 2014 · N971FD · Boeing 75728A · Fire Detection
  > MOMENTARY WW FIRE EICAS ALERT & BELL ON TOUCHDOWN, LASTED 1 - 2 SECONDS, COULD NOT DUPLICATE. INSPECTED DETECTOR LOOPS & ELEC CONNECTIONS IN BOTH MLG WW, NO DEFECTS NOTED. ADJUSTMENT TEST OF WW FIRE DETECTION SYS NORMAL IAW MM 26-17-00-5.
- [SDR FDEA201402040254](https://openairdocs.org/sdr/FDEA201402040254.md): Target · out of adjust · Feb 4, 2014 · N971FD · Boeing 75728A · Engine Thrust Reverser
  > ON TAKEOFF ROLL THE RT REVERSER ECAS MESSAGE CAME INTERMITTENT REJECT AT 80 KTS. REVERSER SECURED IN FWD THRUST POSITION. FOUND THE RIGHT LOCK PROX TARGET, TOO FAR AWAY FROM SENSOR. INSTALLED SHIMS ON RIGHT LOCK PROX SENSOR, PER AMM 78-30-00-5-4. GAP IS WI
- [SDR FDEA201308292072](https://openairdocs.org/sdr/FDEA201308292072.md): Guard · failed · Aug 29, 2013 · N971FD · Boeing 75728A · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHT SWITCH GUARD SPRING IS WEAK AND NOT WORKING PROPERLY, MANUAL OPERATION OF THE SWITCH IS NOT EFFECTED. REMOVED BROKEN EMERGENCY LIGHT SWITCH GUARD. REPLACED WITH NEW GUARD. CHECK FUNCTION OF GUARD AND SWITCH ALONG WITH OPS CHECK
- [SDR FDEA201308021754](https://openairdocs.org/sdr/FDEA201308021754.md): Cable · sheared · Aug 2, 2013 · N971FD · Boeing 75728A · Escape Slide
  > DURING OPENING OF RT SIDE ENTRY DOOR, GIRT BAR HUNG UP ON DOOR SILL, SLIDE PARTIALLY DISENGAGED AS WELL AS SAFETY CABLE SHEARED. R & R R1 DOOR SLIDE ASSY REF AMM 25-66-01. ACFT OK TO CONTINUE SERVICE.
- [SDR FDEA201305301140](https://openairdocs.org/sdr/FDEA201305301140.md): Latch · broken · May 30, 2013 · N971FD · Boeing 75728A · Escape Slide
  > DOOR ESCAPE SLIDE COVER LOWER STRAP LATCH BROKEN. REPLACED LATCH IAW AMM 25-66-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201304180801](https://openairdocs.org/sdr/FDEA201304180801.md): Slider · disconnected · Apr 18, 2013 · N971FD · Boeing 75728A · Emergency Equipment
  > RT FWD ENTRY DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN DOOR ARMED. INSPECTED AND FOUND R1 DOOR GIRT BAR SLIDERS NOT ATTACHED TO DOOR MECHANISM. REINSTALLED GIRT BAR SLIDERS IAW AMM 25-66-01-4. LUBRICATED SLIDER AREA IAW AMM 12-21-18-3. CHECKED OPERATION O
- [SDR FDEA201303040496](https://openairdocs.org/sdr/FDEA201303040496.md): Lamp · inoperative · Mar 4, 2013 · N971FD · Boeing 75728A · Emergency Lighting
  > EMERGENCY EXTERIOR LIGHT AFT OF R1 DOOR INOPERATIVE. REPLACED LAMP IAW SMP'S. OPS CHECKED GOOD.
- [SDR FDEA201301180134](https://openairdocs.org/sdr/FDEA201301180134.md): Skin · corroded · Jan 18, 2013 · N971FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BS 1200 -1220 BETWEEN STRINGER 29 LT AND 29 RT. THERE IS CORROSION AROUND THE TOILET SERVICING HOLES IN THE SKIN. REPAIR CARRIED OUT AS PER EA F-3830-163852. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
- [SDR FDEA201301180133](https://openairdocs.org/sdr/FDEA201301180133.md): Skin · corroded · Jan 18, 2013 · N971FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > AFT CARGO LOWER COMPARTMENT INTERIOR SKIN BETWEEN BS 1200 AND 1205 NEAR LBL 2. CUT OUT AREA WITH CORROSION. REPAIR CARRIED OUT IAW EA F-3830-163852. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
- [SDR FDEA201301180136](https://openairdocs.org/sdr/FDEA201301180136.md): Channel · damaged · Jan 18, 2013 · N971FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MAIN DECK -DURING OK TO INSTALL, FOUND SPLICE CHANNEL WITH ELONGATED HOLE AT STR 1, BS 1620. REMOVED CHANNEL IAW SRM 51-40-02 REV 107. NEW CHANNEL FABRICATED IAW DWG 146N3820 SHT 1 REV C. CHANNEL INSTALLED IAW DWG 146N3106 SHT 1 REV E. REPAIR CLASSIFIED
- [SDR FDEA201301130090](https://openairdocs.org/sdr/FDEA201301130090.md): Stiffener · sheared · Jan 13, 2013 · N971FD · Boeing 75728A · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT RT SIDE LOWER FLOORBEAM STIFFENER STRAP IS BROKEN, BS 1640, RBL 45. COMPLIED PART 1 OF EA F-5330-163846. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201301110067](https://openairdocs.org/sdr/FDEA201301110067.md): Floorbeam · corroded · Jan 11, 2013 · N971FD · Boeing 75728A · Fuselage Main, Floor Beam
  > BS 1320, FLOORBEAM UPPER TEE HAS CORROSION, LBL 56 TO LBL 64. COMPLIED WITH EA F-5310-163824, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201212244372](https://openairdocs.org/sdr/FDEA201212244372.md): Skin · dented · Dec 24, 2012 · N971FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1620, BELOW STR 24R. REPAIR CARRIED OUT IAW EA F-5330-163828. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201212144300](https://openairdocs.org/sdr/FDEA201212144300.md): Crease Beam · corroded · Dec 14, 2012 · N971FD · Boeing 75728A · Fuselage Main, Structure
  > BS 1259, RBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-30-13, ALLOWABLE DAMAGE 1, FIG 101, REV 107. REPAIR CARRIED OUT IAW EA F-5310-162909.
- [SDR FDEA201212124285](https://openairdocs.org/sdr/FDEA201212124285.md): Seat Track · corroded · Dec 12, 2012 · N971FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1050 TO 1075, RBL 24 HAS DEEP DRILL MARK WITH CORROSION ON CHANNEL. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIG.201 REPAIR 4 REV.107. REPAIR MAJOR.

Next page: https://openairdocs.org/aircraft/N971FD/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 = 'N971FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N971FD/reports

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