# Service difficulty reports: N970FD

A list on [N970FD](https://openairdocs.org/aircraft/N970FD.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 · 70 reports

- [SDR FDEA202605050561](https://openairdocs.org/sdr/FDEA202605050561.md): Module · faulted · May 5, 2026 · N970FD · Boeing 75728A · Landing Gear Door Retract Section
  > AFTER TAKEOFF, GEAR DISAGREE AND GEAR DOORS EICAS MESSAGES APPEARED ACCOMPANIED BY AN AUDIBLE AND TACTILE INDICATION THAT THE GEAR AND/OR GEAR DOORS WERE NOT RETRACTED. APPROXIMATELY 3 MINUTES LATER ALL EICAS MESSAGES AND ACCOMPANYING INDICATORS CEASED. A
- [SDR FDEA202506030833](https://openairdocs.org/sdr/FDEA202506030833.md): Skin · cracked · Jun 3, 2025 · N970FD · Boeing 75728A · Leading Edge Devices
  > L/T WING # 2 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF O/B MAIN TRACK TRIMMED DAMAGE AREA, LH WING # 2 SLAT O/B MAIN TRACK IAW B757 SRM 57-43-01-2R FIG 201 REP 4, FORMED, TRIMMED, LOCATE, DRILLED AND INSTALLED REPAIR PARTS IAW B757 SRM 57-4
- [SDR FDEA202506030832](https://openairdocs.org/sdr/FDEA202506030832.md): Skin · cracked · Jun 3, 2025 · N970FD · Boeing 75728A · Leading Edge Devices
  > LE SLAT NO 9 INTERNAL SKIN WITH CRACK REMOVED L/E SLAT NO 9 INTERNAL SKIN PANEL IAW B757 SRM 51-40-02-0G, FORMED TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SKIN PANEL IAW B757 SRM 51-40-02-0G AND BOEING DWG # 114N4076 REV C.
- [SDR FDEA202506030831](https://openairdocs.org/sdr/FDEA202506030831.md): Skin · cracked · Jun 3, 2025 · N970FD · Boeing 75728A · Leading Edge Devices
  > L/T WING # 1 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF I/B MAIN TRACK TRIMMED OUT DAMAGE AREA L/T WING # 1 SLAT ON SKIN AT I/B MAIN TRACK IAW B757 SRM 57-43- 01-2R FIG 201 REP 4, FORMED, TRIMMED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAW
- [SDR FDEA202506030830](https://openairdocs.org/sdr/FDEA202506030830.md): Skin · cracked · Jun 3, 2025 · N970FD · Boeing 75728A · Leading Edge Devices
  > LE SLAT NO 8 INTERNAL SKIN WITH CRACK REMOVED SKIN PANEL L/E SLAT NO 8 IAW B757 SRM 51-40-02-0G FORMED, TRIMMED, LOCATED DRILLED AND INSTALL NEW SKIN PANEL IAW BOEING DWG # 114N4077 REV D AND B757 SRM 51-40- 02-0G.
- [SDR FDEA202307281329](https://openairdocs.org/sdr/FDEA202307281329.md): Unknown · unknown · Jul 28, 2023 · N970FD · Boeing 757200 · Fuselage Main, Attach Fittings
  > R-3 DOOR, STRINGER CLIP DEFORMED AT STRINGER S-13R BETWEEN BS 1340 AND BS 1360. REMOVED AND REPLACED DEFORMED STRINGER CLIP IAW B757 SRM 51-40-02 AND BACDWG 146N6313 REV. C FABRICATION ON NR N00269
- [SDR FDEA202307261306](https://openairdocs.org/sdr/FDEA202307261306.md): Retainer · cracked · Jul 26, 2023 · N970FD · Boeing 757200 · Landing Gear Doors
  > R/H MLG TRUNNION DOOR SEAL RETAINER IS CRACKED.. REMOVED SEAL AND RETAINER, FABRICATED NEW RETAINER PER BAC DWG 113N8200 AND FEDEX EA # F-3210- T0375397 TITLE: LANDING GEAR - MAIN GEAR AND DOORS - RH MLG TRUNNION FAIRING DOOR, SEAL RETAINER, ALTERNATE FINI
- [SDR FDEA202307251292](https://openairdocs.org/sdr/FDEA202307251292.md): Slat · delaminated · Jul 25, 2023 · N970FD · Boeing 757200 · Leading Edge Devices
  > #3 SLAT UPPER SURFACE TRAILING EDGE WEDGE HAS AN AREA OF DISBOND LOCATED 52" FROM THE OUTBOARD EDGE AND 4" FROM THE TRAILING EDGE. APPROX 2.5" IN DIAMETER. REPAIRED #3 SLAT SURFACE TRAILING EDGE WEDGE 2 EA DAMAGED AREAS IAW B757 SRM 51-10- 02, 57-43-02-0I,5
- [SDR FDEA202307201254](https://openairdocs.org/sdr/FDEA202307201254.md): Unknown · unknown · Jul 20, 2023 · N970FD · Boeing 757200 · Fuselage Structure (General)
  > MAIN CABIN - FLOOR PANEL AT STA 440 TO STA 560, LBL24 TO LBL 45 IS SATURATED IN HYDRAULIC FLUID REMOVED, FABRICATED AND REPLACED FLOOR PANEL IAW B757 AMM 53-01-01-4 AND DWG SRZ- 25-005 REV R
- [SDR FDEA202211012702](https://openairdocs.org/sdr/FDEA202211012702.md): Skin · damaged · Nov 1, 2022 · N970FD · Boeing 75728A · Nacelle/Pylon, Plate/Skin
  > WHILE WORKING #1 O/B T/R C DUCT CHANGE FOUND DAMAGE ON UPPER PORTION OF INBOARD #1 ENG FAN COWL REPAIRED IAW EA F-7110-T0371402 THIS IS A MAJOR REPAIR
- [SDR FDEA202204191001](https://openairdocs.org/sdr/FDEA202204191001.md): Collar · cracked · Apr 19, 2022 · N970FD · Boeing 757200 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED AND REPLACED L1 DOOR OPEN LOCK REF AMM 52-11-08-4. OPS CHECK GOOD.
- [SDR FDEA202204191000](https://openairdocs.org/sdr/FDEA202204191000.md): Gust Lock · failed · Apr 19, 2022 · N970FD · Boeing 757200 · Passenger/Crew Doors
  > MDIS 970 52-10 7067 19APR22 DAY OPEN U R1 DOOR HOLD OPEN LOCK COLLAR BROKEN FACT 21APR22 18:02 MEM R1 DOOR HOLD OPEN LOCK (MPN: 654N0244-8) REPLACED
- [SDR FDEA202203300780](https://openairdocs.org/sdr/FDEA202203300780.md): Valve · none · Mar 30, 2022 · N970FD · Boeing 757 · Air Intake Anti/De-Ice System
  > L-ENG ANT-ICE EICAS MESSAGE DISPLAYED ALONG WITH VALVE LIGHT ON L ENGINE ANTI ICE SWITCH DISPLAYED DURING DESCENT WHEN SELECTED ON AND STAYED ON FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED L ENGINE ANTI-ICE VALVE M/M 30
- [SDR FDEA202101160132](https://openairdocs.org/sdr/FDEA202101160132.md): Valve · inoperative · Jan 16, 2021 · N970FD · Boeing 75728A · Landing Gear Brake System
  > NR 5 BRAKE INOPERABLE FUNCTIONS NORMALLY IN ALTERNATE (LT HYD SYS). REPLACED LEFT ANTISKID SHUTTLE VALVE MODULE, IAW 757 MM 32-42-07-4. OPERATIONS AND LEAK CHECK GOOD.
- [SDR FDEA202010230330](https://openairdocs.org/sdr/FDEA202010230330.md): Case · corroded · Oct 23, 2020 · N970FD · Boeing 75728A · Turbine Engine Compressor Section
  > #1 ENG AT 9 O`CLOCK LP COMPRESSOR CASE OUTER SURFACE HAS CORROSION IN EXCESS OF 10 AROUND (FWD) MATING FLANGE TO INLET (UNDER KEVLAR WRAP). REMOVED AND REPLACED #1 ENGINE.
- [SDR FDEA202007081461](https://openairdocs.org/sdr/FDEA202007081461.md): Gust Lock · malfunctioned · Jul 8, 2020 · N970FD · Boeing 75728A · Passenger/Crew Doors
  > L ENTRY DOOR GUST LOCK DOES NOT LATCH IN THE RELEASE POSITION.
- [SDR FDEA201907091515](https://openairdocs.org/sdr/FDEA201907091515.md): Bracket · damaged · Jul 9, 2019 · N970FD · Boeing 75728A · Trailing Edge Flaps
  > WIC 5782600-00-01 AGING AIRCRAFT INSPECTION- LT I/B MAIN FLAP O/B SIDE OF #3 FLAP TRACK FWD BRACKET HAS ELONGATED HOLES. REMOVED,FABRICATED AND INSTALLED NEW BRACKET AT LT I/B MAIN FLAP O/B SIDE OF #3 FLAP TRACK IAW DWG 113N1767 REV.A & E.
- [SDR FDEA201907011451](https://openairdocs.org/sdr/FDEA201907011451.md): Floor Support · corroded · Jul 1, 2019 · N970FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA.1680-1720, BL.0 - RBL.54 FLOOR SUPPORT WEB CORRODED. REMOVED CORROSION FROM M/C AFT DECK WEB STA.1680 - 1720, BL.0 - RBL.54, MAX MATERIAL LOSS AT RBL.46 STA.1680, ORIGINAL THICK..071, MATERIAL LOSS.015, REMAIN. MATERIAL RBL.46.056, A
- [SDR FDEA201907011449](https://openairdocs.org/sdr/FDEA201907011449.md): Skin · corroded · Jul 1, 2019 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > CORROSION, APU LT ACCESS DOOR FUSELAGE CUTOUT STRUCTURE FWD END, APPROX. BS.1887.5, INNER SURFACE, JUST AFT OF THE APU FIREWALL. COMPLIED WITH EA#F-5330-T0347755 P1. FUSELAGE-PLATES & SKINS- CORROSION AT STA.1885, S-17L.
- [SDR FDEA201907011442](https://openairdocs.org/sdr/FDEA201907011442.md): Floorbeam · corroded · Jul 1, 2019 · N970FD · Boeing 75728A · Fuselage Main, Floor Beam
  > COCKPIT STA.345 BETWEEN LBL5-LBL 24 FLOORBEAM CORRODED. CORROSION ON EXISTING FLOORBEAM "T "CAP REPAIR OUT OF LIMITS, REMOVED EXISTING "T" CHORD ANGLE & REPAIR SPLICES, CUT OUT FLOORBEAM FROM RBL.12 TO RBL.53,FABRICATED NEW "T" CHORD & REPAIR PARTS & INSTALLED
- [SDR FDEA201907011450](https://openairdocs.org/sdr/FDEA201907011450.md): Skin · corroded · Jul 1, 2019 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > CORROSION APU RT ACCESS DOOR FUSELAGE CUTOUT STRUCTURE FWD END, APPROX. BS.1887.5, INNER SURFACE, JUST AFT OF THE APU FIREWALL. EVAL. CORROSION DAMAGE WITH 100% MATERIAL LOSS OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 53-80-01-2
- [SDR FDEA201907011448](https://openairdocs.org/sdr/FDEA201907011448.md): Frame · gouged · Jul 1, 2019 · N970FD · Boeing 75728A · Fuselage Main, Frame
  > INSIDE FWD ACC. COMPARTMENT, FRAME AT STA. 231.25 HAS A GOUGE IN UPPER RADIUS AT BL.0. CUT OUT DAMAGE & FABRICATED AND INSTALLED FRAME REPAIR AT STA. 231.25 BL.0 LOWER FRAME SECTION INSIDE FWD ACC. COMPARTMENT IAW SRM 53-00-07-2R, REPAIR 7 FIG 202.
- [SDR FDEA2019021430395](https://openairdocs.org/sdr/FDEA2019021430395.md): Handle · obstructed · Feb 13, 2019 · N970FD · Boeing 75728A · Service Doors
  > COULD NOT ARM SLIDE ON RIGHT HAND ENTRY DOOR. RELOCATED CORD DIDN'T LET CLOSE PROPERLY, OPERATE DOOR SEVERAL TIMES, OPS CKS NORMAL REF AMM 52-11-01-6.
- [SDR FDEA201806071418](https://openairdocs.org/sdr/FDEA201806071418.md): Static Line · tangled · Jun 7, 2018 · N970FD · Boeing 75728A · Emergency Equipment
  > RIGHT FORWARD ENTRY DOOR WILL NOT FULLY DISARM. SLIDE ARM LIGHT WILL EXTINGUISH, BUT EVACUATION SLIDE LEVER WILL NOT MOVE FULLY TO THE DISARM POSITION. FOUND STATIC LINE TANGLED ON THE FORWARD PART OF THE GIRT BAR, RESTOWED STATIC LINE. PERFORMED OPS CHEC
- [SDR FDEA201709222674](https://openairdocs.org/sdr/FDEA201709222674.md): Plunger · damaged · Sep 22, 2017 · N970FD · Boeing 75728A · Cargo/Baggage Doors
  > RAMP REPORTED THE MAIN CARGO DOOR WILL NOT CLOSE. FOUND THE TIP MISSING FROM PLUNGER ON MAIN CARGO DOOR SEQUENCE VALVE. REPLACED THE TIP IAW SRM 51-40-02. MAIN CARGO DOOR CHECKED GOOD IAW 52-32-00-2. ACFT OK FOR SERVICE.
- [SDR FDEA201705241502](https://openairdocs.org/sdr/FDEA201705241502.md): Bottle · empty · May 24, 2017 · N970FD · Boeing 75728A · Passenger/Crew Doors
  > L1 DOOR WAS ARMED, CREW ATTEMPTED TO OPEN DOOR, L1 EMERGENCY ASSIST BOTTLE DEPLETED SLIDE DID NOT DEPLOY.
- [SDR FDEA201612114381](https://openairdocs.org/sdr/FDEA201612114381.md): Warning Light · false activation · Dec 11, 2016 · N970FD · Boeing 75728A · Fuel Boost Pump
  > AT LEVEL OFF, RECEIVED A CTR L FUEL PUMP ALERT WITH 5.1 OF FUEL IN CENTER TANK. REACTIVATED LT CTR OVERRIDE FUEL PUMP. AUDIBLE CHECKED THE LT CTR OVERRIDE PUMP FOR OPERATION, PUMP IS RUNNING. TRANSFERRED 22 KLBS INTO CENTER FUEL TANK. LT CTR OVERRIDE PUM
- [SDR FDEA201609213326](https://openairdocs.org/sdr/FDEA201609213326.md): Window · failed · Sep 21, 2016 · N970FD · Boeing 75728A · Flight Compartment Windows
  > AT CRUISE FL290, A LOUD BANG WAS HEARD THEN ARCING & SHATTERING OF FO'S FORWARD WINDOW. REPLACED RT FWD WINDOW. OK FOR SERVICE.
- [SDR FDEA201507212287](https://openairdocs.org/sdr/FDEA201507212287.md): Fseu · inoperative · Jul 21, 2015 · N970FD · Boeing 75728A · Leading Edge Slat Control System
  > ON DEPARTURE, WHEN SELECTING FLAPS UP, HAD A LE DISAGREE EICAS. FLAP INDICATOR SHOWED STUCK BETWEEN 1 DEGREE & UP. PERFORMED CHECKLIST & RETURNED TO DEPARTURE. R & R FSEU IN NR 1 POSITION. OPS CHECKED IAW AMM 27-51-01-2 PAGE 1-16. FLAPS & SLATS OPERATED N
- [SDR FDEA201506201930](https://openairdocs.org/sdr/FDEA201506201930.md): Skin · dented · Jun 20, 2015 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > PROTRUDING DENT STATION 523 AT STRINGER 26L. COMPLIED WITH EA F-5330-TO318148 PART 1 FUSELAGE PLATES & SKIN. REPAIR AT STATION 523 BETWEEN STRINGERS 26L - 27L.
- [SDR FDEA201506201929](https://openairdocs.org/sdr/FDEA201506201929.md): Skin · dented · Jun 20, 2015 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > TWO EACH DENTS STATION 490 BELOW 27L. COMPLIED WITH EA F-5330-TO318149 PART 1 FUSELAGE PLATES & SKINS. REPAIR AT STATION 490 BETWEEN STRINGERS 27L - 28L.
- [SDR FDEA201506161821](https://openairdocs.org/sdr/FDEA201506161821.md): Skin · dented · Jun 16, 2015 · N970FD · Boeing 75728A · Ailerons
  > LEFT AILERON UNDER SIDE HAS SMALL DENT. BONDED REPAIRED IAW SRM 51-70-17 PG 14/15 PARA 4, 57-60-01-212. OPS CHECKED GOOD IAW AMM 27-11-00-0.
- [SDR FDEA201312203031](https://openairdocs.org/sdr/FDEA201312203031.md): Bolt · out of position · Dec 20, 2013 · N970FD · Boeing 75728A · Leading Edge Slat Control System
  > AFTER LANDING GOT FLAP LE SLAT AYSYM EICAS MESSAGE BETWEEN UP & 1 POSITION. NR 1 FLAP, SLAT ELEX UNIT BITE SHOWS RT SLAT DRIVE. NR 2 UNIT SHOWS RT SLAT XMITTER. TROUBLESHOT IAW FIM 27-51. FAULT TREE 805, FOUND NR 6 LE SLAT CTR OTBD TORQUE TUBE DRIVE SPLINE
- [SDR FDEA201308081809](https://openairdocs.org/sdr/FDEA201308081809.md): Wire · loose · Aug 8, 2013 · N970FD · Boeing 75728A · Light System Wiring
  > EMERGENCY EXIT SIGN ABOVE R1 DOOR INOPERATIVE. FOUND R1 DOOR EMERGENCY EXIT LIGHT WIRE NR 1 NOT PROPERLY SEATED AT QUICK DISCONNECT, RESEATED WIRE IAW SMP. R1 DOOR EMERGENCY EXIT LIGHT OPS CHECKED GOOD IAW MM 33-51-01-2. ACFT OK FOR SERVICE.
- [SDR FDEA201307231638](https://openairdocs.org/sdr/FDEA201307231638.md): Battery Pack · inoperative · Jul 23, 2013 · N970FD · Boeing 75728A · Emergency Lighting
  > SLIDE ILLUMINATION LIGHT AND CENTER EMERGENCY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY ASSY IAW AMM 33-51-07-2. OPS CHECKED GOOD.
- [SDR FDEA201306251413](https://openairdocs.org/sdr/FDEA201306251413.md): Skin · cracked · Jun 25, 2013 · N970FD · Boeing 75728A · Leading Edge Devices
  > LT WING NR 3 SLAT, AT INBD TRACK, JUST OUTBOARD, COVE SKIN CRACKED, COVE SKIN FOUND TO BE OUT OF LIMITS IAW-SRM-57-43-01, FIG 101, SHEET (2 OF 4) NOTE B, NO CRACKS ALLOWED. REMOVED COVE SKIN AT LT WING NR 3 SLAT OSS 471.30-483.30. FABRICATED NEW COVE SKIN O
- [SDR FDEA201306131370](https://openairdocs.org/sdr/FDEA201306131370.md): Crease Beam · cracked · Jun 13, 2013 · N970FD · Boeing 75728A · Fuselage Main, Structure
  > CREASE BEAM OTBD ANGLE CRACKED AT BS 1641, S17L. REPAIRED CREASE BEAM IAW EA 757-5361-16-F4175. MAJOR REPAIR.
- [SDR FDEA201306131271](https://openairdocs.org/sdr/FDEA201306131271.md): Skin · debonded · Jun 13, 2013 · N970FD · Boeing 75728A · Trailing Edge Flaps
  > LEFT WING INBD FLAP, TOP OTBD PANEL LOWER SURFACE, DISBONDED. REPAIRED SKIN IAW SRM 51-70-10. REPAIR 4. MAJOR REPAIR
- [SDR FDEA201305311154](https://openairdocs.org/sdr/FDEA201305311154.md): Skin · misrepaired · May 31, 2013 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BS 395-418 BETWEEN S2-4L MISREPAIRED. REPAIRED IAW EA F-5330-T0300578. MAJOR REPAIR
- [SDR FDEA201305311153](https://openairdocs.org/sdr/FDEA201305311153.md): Stringer Fitting · corroded · May 31, 2013 · N970FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > LOWER LOBE STR 26L AFT END ATTACHMENT FITTING HAS CORROSION BS 1720. REMOVED CORROSION ON STRINGER 26L END FITTING IAW SRM 51-10-02, ORIGINAL THICKNESS.090, REMAINING THICKNESS.066, NO SRM ALLOWABLE LIMITS. R & R END FITTING IAW DWG 146N8849, SH 1 REV- AND
- [SDR FDEA201305221068](https://openairdocs.org/sdr/FDEA201305221068.md): Skin · damaged · May 22, 2013 · N970FD · Boeing 75728A · Trailing Edge Flaps
  > RT WING INBD FLAP, TOP OTBD PANEL, LOWER SURFACE HONEYCOMB EDGE VOID. REPAIRED IAW SRM 51-70-10. REPAIR 4. CAT "A" MAJOR REPAIR.
- [SDR FDEA201305211057](https://openairdocs.org/sdr/FDEA201305211057.md): Fitting · worn · May 21, 2013 · N970FD · Boeing 75728A · Fuselage Main, Attach Fittings
  > BS 935, BL 0, FITTING HAS ONE OVERSIZED HOLE OF 0.352 IN DIAMETER. THE MATING FLOOR STRUCTURE HAS SAME HOLE SIZE AT SAME LOCATION AT STA 935, BL0. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM W/C 49925760001 AND (STAM) EA
- [SDR FDEA201305161011](https://openairdocs.org/sdr/FDEA201305161011.md): Skin · dented · May 16, 2013 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN BS 1600-1620 BETWEEN S25-26R HAS TWO DENTS.. BS 1613 BETWEEN S26-25R A=0.6 Y=.045 A/Y= 13.33 OUT OF LIMITS. REPAIRED IAW SRM-53-00-01, FIG 201, REPAIR NR 7. MAJOR REPAIR.
- [SDR FDEA201305151005](https://openairdocs.org/sdr/FDEA201305151005.md): Skin · corroded · May 15, 2013 · N970FD · Boeing 75728A · Leading Edge Devices
  > NR 1 SLAT COVE SKIN LWR EDGE CORRODED. REMOVED CORROSION IAW-SRM-51-10-02 ON NR 1 SLAT COVE SKIN LWR EDGE, CHECKED LIMIT.050 MAT. LOSS.009, FOUND OUT OF LIMITS, IAW- SRM-57-43-01, FIG 101, SHEET 4, DET IV, R & R COVE SKIN IAW-SRM-51-40-02 AND DWG 114N4075
- [SDR FDEA201305140982](https://openairdocs.org/sdr/FDEA201305140982.md): Fitting · cracked · May 14, 2013 · N970FD · Boeing 75728A · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON STRUT TO DIAGONAL BRACE FITTING RT SIDE AFT INBD HOLE SHOWS CRACK INDICATION AT THE 4:30 POS IN THE ALUMINUM BULKHEAD ONLY. COMPLIED WITH EA F-5450-T0300259THIS IS A MAJOR REPAIR AND IS CONSIDERED CATAGORY "A".
- [SDR FDEA201305100969](https://openairdocs.org/sdr/FDEA201305100969.md): Skin · misrepaired · May 10, 2013 · N970FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > SKIN MISREPAIRED BS 1700 -1720 S15-16L. REPAIRED IAW EA F-5330-T0300418, CAT "B" MAJOR REPAIR.
- [SDR FDEA201305070932](https://openairdocs.org/sdr/FDEA201305070932.md): Skin · gouged · May 7, 2013 · N970FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE EXTERNAL SKIN HAS GOUGES AT STA. 1862, S9L.
- [SDR FDEA201304270871](https://openairdocs.org/sdr/FDEA201304270871.md): Frame · cracked · Apr 27, 2013 · N970FD · Boeing 75728A · Fuselage Main, Frame
  > MAIN CABIN BS 760 BETWEEN S8- 9R FRAME IS CRACKED. FOUND CRACKED AT FAST HOLE, CRACKED IS NOT ALLOWED IAW SRM 53- 00-07, REPAIRED FRAME IAW SRM 53-00-07, REPAIR 3. MAJOR REPAIR.
- [SDR FDEA201304240849](https://openairdocs.org/sdr/FDEA201304240849.md): Skin · cracked · Apr 24, 2013 · N970FD · Boeing 75728A · Leading Edge Devices
  > NR 2 SLAT COVE SKIN, OSS 677.5 CRACKED AT FASTENER. REMOVED CRACKED NR 2 SLAT COVE SKIN IAW-SRM-51-40-02, REPLACED CRACKED COVE SKIN WITH NEW COVE SKIN IAW-SRM-51-40-02 AND DWG 114N4076, CAT"A" MAJOR REPAIR.
- [SDR FDEA201304230834](https://openairdocs.org/sdr/FDEA201304230834.md): Skin · cracked · Apr 23, 2013 · N970FD · Boeing 75728A · Leading Edge Devices
  > NR 1 SLAT COVE SKIN, OSS 736.7, CRACKED AT FASTENER. REMOVED CRACKED NR 1 SLAT COVE SKIN, IAW-SRM-51-40-02, FOUND OUT OF LIMITS, IAW-53-00-71. REPLACED CRACKED COVE SKIN WITH NEW COVE SKIN, IAW-SRM-51-40-02 AND 757 DWG 114N4075, NR 1 SLAT- O.S.S. -736.7 TO

Next page: https://openairdocs.org/aircraft/N970FD/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 = 'N970FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N970FD/reports

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