# Service difficulty reports: N922FT, cancelled Apr 23, 2009

A list on [N922FT, cancelled Apr 23, 2009](https://openairdocs.org/deregistered/N922FT-2009-04-23.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 · 59 reports

- [SDR WRNA200600018](https://openairdocs.org/sdr/WRNA200600018.md): Engine · malfunctioned · Jun 6, 2006 · N922FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, A BALL OF FIRE FROM THE LEFT SIDE WAS REPORTED ACCOMPANIED WITH A LOUD BANG, CREW BELIEVED NR 1 ENGINE HAD FAILED AND ABORT OF TAKEOFF WAS INITIATED. AIRCRAFT SKIDDED APPROX 150 FEET OFF END OF RUNWAY, (RUNWAY CONTAMINATED WITH STANDING WATER)
- [SDR WRNA200600014](https://openairdocs.org/sdr/WRNA200600014.md): Static Line · broken · May 25, 2006 · N922FT · Boeing 7472U3B · Pitot/Static System
  > RUDDER RATIO LIGHT CAME ON IN CLIMB,.84M SPEED 300K ALT 32,000. STAYED -ON- CRUISE 39,000 AT 261K, UPPER RUDDER 2 DEGREES LEFT, LOWER RUDDER 0 DEGREES, LIGHT WENT OUT AT 24,000 AT 300K. RETURNED TO MIA AND MADE A SAFE LANDING. RIGGED UPPER AND LOWER RUDDER
- [SDR WRNA200600005](https://openairdocs.org/sdr/WRNA200600005.md): Filter · unknown · Feb 26, 2006 · N922FT · Boeing 7472U3B · Engine Fuel and Control
  > WHEN LEVELING FL 380, MACH SPD.84, WHILE SLOWLY REDUCING POWER, NR 1 ENGINE AUDIBLY COMPRESSOR STALLED, EPR FLUX ALONG WITH INCREASE IN EGT, AMBER/HIGH EGT LIGHT ILLUMINATED, UPON REDUCING NR 1 ENG TO IDLE, EPR CONTINUED TO FLUX, ACCOMPLISHED ENGINE FAILURE/P
- [SDR WRNA200500018](https://openairdocs.org/sdr/WRNA200500018.md): Line · unserviceable · Jul 3, 2005 · N922FT · Boeing 7472U3B · Hydraulic System, Main
  > T/O FROM TPE, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. AIRCRAFT RETURNED TO BASE, LANDING NORMAL. FOUND HYDRAULIC LINE TO TRUCK POSITION ACTUATOR LEAKING (BLOWN). REMOVED AND REPLACED LINE IAW 32-13-05, OP'S CHECK SATISFACTORY, NO LEAKS NOTED. A/
- [SDR WRNA200500016](https://openairdocs.org/sdr/WRNA200500016.md): Engine · damaged · Jun 21, 2005 · N922FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > VERY LOUD RUMBLE ON TAKE OFF. UPON LANDING, NR 2 ENGINE WAS FOUND TO HAVE COILS MISSING FROM LT SIDE. RT SIDE DAMAGED, ALONG WITH VARIOUS OTHER AREAS OF DAMAGE TO DUCT WORK, FIRE SEAL, AND HYD RACEWAY. ALL ITEMS WERE REPAIRED/REPLACED IAW MM 72-11-02,75-24-
- [SDR WRNA200500013](https://openairdocs.org/sdr/WRNA200500013.md): Engine · damaged · May 21, 2005 · N922FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > NR1 ENGINE COMPRESSOR STALLED AT FL 11.5, AIRCRAFT RETURNED. LANDING NORMAL. ENGINE BOROSCOPE COMPLIED WITH, NO DISCREPANCIES NOTED. NR 1 ENGINE FAN CASING ACOUSTIC LINERS FROM 1O`CLOCK TO 8 O'CLOCK POSITION DAMAGED. REMOVED AND REPLACED PANELS IAW 72-31-08,
- [SDR P5CA0401032](https://openairdocs.org/sdr/P5CA0401032.md): Pushrod · sheared · Jan 29, 2004 · N922FT · Boeing 7472U3B · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR FWD HOOK SHAFT PUSH ROD SHEARED ON OPEN SEQUENCE. INSTALLED FWD HOOK SHAFT PUSH ROD, OPS NORMAL IAW 52-32-11.
- [SDR P5CA0401017](https://openairdocs.org/sdr/P5CA0401017.md): Pushrod · broken · Dec 23, 2003 · N922FT · Boeing 7472U3B · Cargo/Baggage Doors
  > SIDE CARGO DOOR FAILS TO OPEN. FOUND PUSH ROD BROKEN HOOK ACTUATOR FWD SIDE. REMOVED AND REPLACED ROD AS PER MM 52-32-00, OPS CHECK, OPERATION CHECK NORMAL.
- [SDR P5CA0301016](https://openairdocs.org/sdr/P5CA0301016.md): Skin · damaged · Dec 21, 2003 · N922FT · Boeing 7472U3B · Cargo/Baggage Doors
  > MAIN DECK CRG DOOR FAILED TO CLOSE - DOOR SKIN DAMAGED. PERFORMED TIME LIMITED REPAIR TO DOOR IAW SL TLS-JFK 03-00243H AND SRM COI WAS ISSED AND DOOR DEFERRED ELECTRICALLY IAW DDPG.
- [SDR P5CA0301009](https://openairdocs.org/sdr/P5CA0301009.md): Rod · defective · Dec 19, 2003 · N922FT · Boeing 7472U3B · Cargo/Baggage Doors
  > SIDE CARGO DOOR FAILS TO CLOSE. REPLACED INPUT ROD TO FWD HOOK TORQUE TUBE IAW 52-32-11.
- [SDR P5CA0300991](https://openairdocs.org/sdr/P5CA0300991.md): Engine · failed · Nov 16, 2003 · N922FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED IN FLT LOUD RUMBLE FOLLOWED BY LOSS OF POWER HIGH EGT VIBRATION OIL LOSS. REPLACED NR 2 ENG PER MM 71-00-002.
- [SDR P5CA0300977](https://openairdocs.org/sdr/P5CA0300977.md): Frame · damaged · Oct 31, 2003 · N922FT · Boeing 7472U3B · Fuselage Main, Frame
  > MAIN DECK CARGO AREA, FUSELAGE FRAME, STA 1700 RT SIDE S-1 TO S-11 FRAME DAMAGE. REMOVED DAMAGED PORTION OF FRAME SECTION. REPAIR ACCOMPLISHED IAW SRM 53-10-04.
- [SDR P5CA0300956](https://openairdocs.org/sdr/P5CA0300956.md): Skin · cracked · Sep 22, 2003 · N922FT · Boeing 7472U3B · Trailing Edge Flaps
  > RT OUTBOARD MID FLAP COVE PNL DELAMINATED / CRACKED - 24 INCH LONG - WBL 660. REPAIRED DAMAGE AREA
- [SDR P5CA0300933](https://openairdocs.org/sdr/P5CA0300933.md): Pump · leaking · Aug 31, 2003 · N922FT · Boeing 7472U3B · Hydraulic Pump (Electric/Engine), Main
  > LOSS HYD FLUID NR 4 SYS. NR 4 EDP REMOVED AND DEACTIVATED INSTALLED DEACTIVATION KIT IAW MEL 29-01-A TRASFERRED TO DMI 31340.
- [SDR P5CA0300924](https://openairdocs.org/sdr/P5CA0300924.md): Hydraulic Line · ruptured · Aug 24, 2003 · N922FT · Boeing 7472U3B · Hydraulic System, Main
  > NR 1 HYDRAULIC SYS QUANITITY AND PRESSURE DROPPED TO ZERO AT STARTUP. SWAPPED PRESSURE LINE FROM NR 2 TO NR 1. CAPPED NR 2 ADP LINE FITTINGS. PERFORMED LEAK CHECKS, OPERATIONAL CHECK PER 29-11-00. SYS OPERATIONAL CHECK AND LEAK CHECK NORMAL.
- [SDR P5CA0300896](https://openairdocs.org/sdr/P5CA0300896.md): Coupling · sheared · Jun 3, 2003 · N922FT · Boeing 7472U3B · Engine Cranking
  > NR N2 INDICATION ON NR 3 ENGINE, DURING START - ENGINE DID NOT START PYLON AND START VALVE LIGHTS SHOW AIR PRESS TO STARTER BUT NO ROTATION. REMOVED AND REPLACED PNUEMATIC STARTER ALSO COUPLING WAS SHEARED.
- [SDR P5CA03000885](https://openairdocs.org/sdr/P5CA03000885.md): Warning Light · illuminated · May 30, 2003 · N922FT · Boeing 7472U3B · Fire Detection
  > ON T/O NR 4 ENG FIRE DET A-LOOP ILLUMINATED FIRE LIGHT. B-LOOP NORMAL. ITEM WAS DEFERRED PER THE DDPG AFTER IT WAS DETERMINED THAT ONE LOOP WAS OPERATIONAL. DEFECTIVE A-LOOP.
- [SDR P5CA0300884](https://openairdocs.org/sdr/P5CA0300884.md): Clamp · loose · May 28, 2003 · N922FT · Boeing 7472U3B · Pneumatic Distribution System
  > BOTH A&B NR 2 NACELLE TEMP SPIKING RETARDED THROTTLE NACELLE INDICATIONS NORMAL. ON LEAK CK FOUND FAILED DUCT CLAMP BETWEEN HEAT EXCHANGER & ENG DUCT. INSTALLED NEW CLAMP AND ON LEAK CHECK NIL LEAKS NOTED. THREADS STRIPPED ON HOLDING BOLT FOR CLAMP.
- [SDR P5CA0300883](https://openairdocs.org/sdr/P5CA0300883.md): Bulkhead · cracked · May 28, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Bulkhead/Firewall
  > CRACKS FOUND ON AFT TORQUE BULKHEAD ON NR 1 & 4 PYLONS. REPAIRED PER SB 54-2201 BOEING PAO R11-03-00004H.
- [SDR P5CA0300882](https://openairdocs.org/sdr/P5CA0300882.md): Bulkhead · cracked · May 28, 2003 · N922FT · Boeing 7472U3B · Fuselage Main, Bulkhead
  > CRACK FOUND ON 1480 LWR BULKHEAD RT SIDE. REPAIRED PER S/B 53-2390.
- [SDR P5CA0300872](https://openairdocs.org/sdr/P5CA0300872.md): Nozzle · leaking · Apr 24, 2003 · N922FT · Boeing 7472U3B · Fuel Dump System
  > DURING FUELING LEAK WAS OBSERVED FROM LT WING FUEL JETTISON NOZZLE VALVE. REPLACED LT FUEL JETTISON NOZZLE VALVE.
- [SDR P5CA0300738](https://openairdocs.org/sdr/P5CA0300738.md): Frame · cracked · Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/Rib
  > CRACK, APPROX. 1", FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FRAME ON HORIZONTAL FLANGE, STARTING FROM TOP EDGE. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.
- [SDR P5CA0300737](https://openairdocs.org/sdr/P5CA0300737.md): Frame · cracked · Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/Rib
  > CRACK 1-1/2" FOUND #3 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FWD FRAME REAPIR ANGLE, STARTING FROM TOP EDGE RADIUS. FRAME REPAIR ANGLE REPLACED PER SRM 54-10-03 & FAA FORM 8110-3.
- [SDR P5CA0300736](https://openairdocs.org/sdr/P5CA0300736.md): Frame · cracked · Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/Rib
  > 5 CRACKS TOTAL FOUND #2 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST FWD FRAME. L/H: (1) 2" CRACK ON L/H SIDE FRAME, STARTING FROM TOP EDGE ON VERTICAL FLANGE. R/H: (3) 1/2" EA. CRACKS ON R/H SIDE, STARTING ON 1ST AFT FASTENER HOLE FROM TOP ON HORIZONTAL FLANGE
- [SDR P5CA0300735](https://openairdocs.org/sdr/P5CA0300735.md): Frame · cracked · Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/Rib
  > CRACK FOUND #1 PYLON REAR ENG. MOUNT BULKHEAD L/H FWD FRAME APPROX. 1/2" FROM TOP RADIUS. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.
- [SDR P5CA0300734](https://openairdocs.org/sdr/P5CA0300734.md): Skin · cracked · Jan 22, 2003 · N922FT · Boeing 7472U3B · Passenger/Crew Doors
  > EVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 L/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO THE VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAIR CARRIED OUT IAW SRM 52-10-02, FIG. 9.
- [SDR P5CA0300733](https://openairdocs.org/sdr/P5CA0300733.md): Skin · cracked · Jan 22, 2003 · N922FT · Boeing 7472U3B · Passenger/Crew Doors
  > EVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 R/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAIR CARRIED OUT IAW SRM 52-10-02, FIG. 9.
- [SDR P5CA0300732](https://openairdocs.org/sdr/P5CA0300732.md): Fitting · corroded · Jan 22, 2003 · N922FT · Boeing 7472U3B · APU Engine Fuel and Control
  > CORROSION LEVEL 1 FOUND ON LINE SHROUD FITTING DURING REMOVAL OF APU FUEL LINE SHROUD FIBERGLASS CLOSE OUT PANEL. NEW SHROUD LINE FITTING INSTALLED & LEAK CHECK CARRIED OUT PER MM 28-25-04. FOUND SATISFACTORY AND NO LEAKS OBSERVED.
- [SDR P5CA0300731](https://openairdocs.org/sdr/P5CA0300731.md): Panel · delaminated · Jan 20, 2003 · N922FT · Boeing 7472U3B · Wing, Plate/Skin
  > DELAMINATION FOUND L/H WING LEADING EDGE TOP PANEL AT FSSD 1550 (O/B MOST). PANEL REPAIR CARRIED OUT PER SRM 51-40-12 & SRM 51-30-20.
- [SDR P5CA0300730](https://openairdocs.org/sdr/P5CA0300730.md): Support Angle · cracked · Jan 20, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Bulkhead/Firewall
  > CRACK APPROX. 2-3/4" FOUND #4 PYLON AFT ENG. BULKHEAD FRAME AT NAC STA 221.90 MID SPARE WEB LWR LATERAL SUPPORT ANGLE AT MID SECTION & JOINTING 3 FASTENERS. REPLACEMENT OF CRACKED LATERAL SUPPORT ANGLE CARRIED OUT PER SRM 51-10-01.
- [SDR P5CA0300729](https://openairdocs.org/sdr/P5CA0300729.md): Frame · cracked · Jan 19, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/Rib
  > CRACK FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD FRAME ASSY BELOW NAC WL 167.0 ON L/H FWD, R/H FWD & AFT AT FASTENER HOLE. REPLACEMENT OF CRACKED FRAME ASSY CARRIED OUT AS PER SRM 51-10-01
- [SDR P5CA0300725](https://openairdocs.org/sdr/P5CA0300725.md): Brace · gouged · Jan 14, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach Fittings
  > NICK/GOUGE FOUND AT SAILBOAT AREA OF PYLON #1 DIAGONAL BRACE - LOCATED APPROX 10:00 O'CLOCK POSITION, 29" FROM FWD END AT ZONE 5. DAMAGED AREA BLEND-OUT CARRIED OUT - FINAL DIMENSION LENGTH 2.0, WIDTH 1.525, DEPTH 0.100. THESE FIGURES ARE WITHIN LIMITS PER BOE
- [SDR P5CA0300724](https://openairdocs.org/sdr/P5CA0300724.md): Stiffener · corroded · Jan 12, 2003 · N922FT · Boeing 7472U3B · Wing Miscellaneous Structure
  > CORROSION LEVEL 1 FOUND R/H WING LEADING EDGE FRONT SPAR "L" STIFFENER AT FSSI 1435 LOWER PORTION. REPAIR CARRIED OUT IAW SRM 51-30-02.
- [SDR P5CA0300723](https://openairdocs.org/sdr/P5CA0300723.md): Stiffener · corroded · Jan 12, 2003 · N922FT · Boeing 7472U3B · Wing Miscellaneous Structure
  > CORROSION LEVEL 1 FOUND LEADING EDGE TOP PANEL SUPPORT RIB AT STA. FSS 1336.00, "L" ANGLE STIFFENER TO FRONT SPAR. "L" ANGLE REPAIR CARRIED OUT AS PER SRM 51-30-02.
- [SDR P5CA0300722](https://openairdocs.org/sdr/P5CA0300722.md): Fitting · cracked · Jan 12, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach Fittings
  > SIX CRACKS TOTAL FOUND NR 4 REAR ENG MOUNT BATHTUB FITTING: I/B FASTENER HOLE HAS 3 CRACKS - (1).125 INCH, (1).1875 INCH & (1).75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1).125 INCH, (1).5 INCH & (1).75 INCH RADIALLY. CRACKED BATHTUB FITTING
- [SDR P5CA0300721](https://openairdocs.org/sdr/P5CA0300721.md): Fitting · cracked · Jan 12, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach Fittings
  > FIVE CRACKS TOTAL FOUND NR 3 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1.5 INCH & (1).75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX.5 INCH & (2).125 INCH EA RADIALLY. CRACKED BATHTUB FITTING
- [SDR P5CA0300720](https://openairdocs.org/sdr/P5CA0300720.md): Fitting · cracked · Jan 12, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach Fittings
  > FIVE CRACKS TOTAL FOUND NR 2 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1 INCH & (1).875 INCH RADIALLY/ O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX.75 INCH & (2) 1 INCH EA RADIALLY. CRACKED BATHTUB FITTING REP
- [SDR P5CA0300718](https://openairdocs.org/sdr/P5CA0300718.md): Fitting · cracked · Jan 9, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach Fittings
  > TWO CRACKS FOUND AROUND INBOARD AND OUTBOARD FASTENER HOLES NR 1 PYLON REAR ENGINE MOUNT BULKHEAD BATHTUB FITTING. - I/B: (1).75 INCH, (1).125 INCH RADIALLY. O/B: (1).75 INCH, (1).5 INCH RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER S/B 747-54-2113 R2
- [SDR P5CA0300728](https://openairdocs.org/sdr/P5CA0300728.md): Rod · corroded · Dec 31, 2002 · N922FT · Boeing 7472U3B · Elevator Control System
  > CORROSION LEVEL 1 FOUND ON L/H INBD ELEVATOR POWER CONTROL PACKAGE ROD END, WITH TEFLON SEAL ADRIFT. POWER CONTROL PACKAGE REPLACED IAW MM 27-31-07.
- [SDR P5CA0200655](https://openairdocs.org/sdr/P5CA0200655.md): Plug · missing · Feb 26, 2002 · N922FT · Boeing 7472U3B · Flight Control System
  > PDU NR 4 DRAIN PLUG MISSING. INSTALLED PLUG AND FILLED PDU IAW 12-13-12. PDU RAN OK.
- [SDR P5CA0200653](https://openairdocs.org/sdr/P5CA0200653.md): Panel · cracked · Feb 26, 2002 · N922FT · Boeing 7472U3B · Wing, Plate/Skin
  > CRACK LT WING REAR SPAR TO INBOARD AILERON TRAILING EDGE UPPER PANEL (573ST). PANEL ASSY REPLACED REF SRM 51-10-01.
- [SDR P5CA0200654](https://openairdocs.org/sdr/P5CA0200654.md): Panel · damaged · Feb 25, 2002 · N922FT · Boeing 7472U3B · Wing, Plate/Skin
  > DAMAGE LT WING UPPER PANEL STATION WS 440.62, ABOVE KRUEGER FLAPS 11/13. NO CRACK FOUND. REPAIR CARRIED OUT WITH REF TO SRM 51-40-09 & 51-40-15.
- [SDR P5CA0100594](https://openairdocs.org/sdr/P5CA0100594.md): Engine · malfunctioned · Sep 20, 2001 · N922FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > WHEN THROTTLES WERE RETARDED FOR DESCENT, NR 2 ENG HAD EXCESSIVE VIBRATION FOLLOWED BY UNCLEARABLE STALL CONDITION. ENG SHUTDOWN WAS ACCOMPLISHED NORMALLY. LUBRICATED BLEED FEEDBACK PUSH PULL CABLE SYSTEM. INSPECTED ENG INLET EXHAUST BLEEDS. OPS CHECKED OK
- [SDR P5CA0100484](https://openairdocs.org/sdr/P5CA0100484.md): Stringer · cracked · Feb 28, 2001 · N922FT · Boeing 7472U3B · Fuselage Main, Longeron/Stringer
  > CRACK 2.1 LONG BS 1000 LHS STR 46. REPAIRED PER SB747-53-2316.
- [SDR P5CA0100480](https://openairdocs.org/sdr/P5CA0100480.md): Intercostal · cracked · Feb 26, 2001 · N922FT · Boeing 7472U3B · Fuselage Miscellaneous Structure
  > CRACK 2.25 INCH FOUND ON INTERCOSTAL BS 434 STR 26. REPAIRED PER SRM 53-30-02.
- [SDR P5CA0100479](https://openairdocs.org/sdr/P5CA0100479.md): Skin · cracked · Feb 26, 2001 · N922FT · Boeing 7472U3B · Fuselage Main, Plate/Skin
  > CRACK FOUND BS 434 STR 26 & 27. REPAIRED PER SRM 53-30-02.
- [SDR P5CA0100478](https://openairdocs.org/sdr/P5CA0100478.md): Skin · cracked · Feb 26, 2001 · N922FT · Boeing 7472U3B · Fuselage Main, Plate/Skin
  > CRACK FOUND AT BS 1000 STR 46-47 RT 1.8 LONG. REPAIRED PER S/B 747-53-2316.
- [SDR P5CA0100477](https://openairdocs.org/sdr/P5CA0100477.md): Skin · corroded · Feb 26, 2001 · N922FT · Boeing 7472U3B · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION BETWEEN STA 1700-1720 STR 50L AND51L. REPAIRED PER 53-30-03.
- [SDR P5CA0100476](https://openairdocs.org/sdr/P5CA0100476.md): Panel · cracked · Feb 26, 2001 · N922FT · Boeing 7472U3B · Fuselage Miscellaneous Structure
  > CRACK FOUND AT CANTED RPESSURE BULKHEAD R/L CLOSURE PANELS AT WEB STA 1240. REPAIRED PER SRM 53-10-02 AND 8110-3 SB 747-53-2329.
- [SDR P5CA0100475](https://openairdocs.org/sdr/P5CA0100475.md): Skin · dented · Feb 26, 2001 · N922FT · Boeing 7472U3B · Fuselage Main, Plate/Skin
  > DENT AT 3 LOCATIONS STA 1830 TO 1840 STR 39L TO 40L. REPAIRED PER SRM 53-30-03.

Next page: https://openairdocs.org/deregistered/N922FT-2009-04-23/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 = 'N922FT' AND deregistration_id = 'N922FT-2009-04-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N922FT-2009-04-23/reports

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