# Service difficulty reports: N923FT, cancelled Dec 21, 2017

A list on [N923FT, cancelled Dec 21, 2017](https://openairdocs.org/deregistered/N923FT-2017-12-21.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 · 66 reports

- [SDR WRNA200800007](https://openairdocs.org/sdr/WRNA200800007.md): Connector · dirty · Mar 15, 2008 · N923FT · Boeing 7472U3B · Air Conditioning System Wiring
  > AFTER TAKEOFF FROM MIA, NR 1 PACK INOP, UNABLE TO MAINTAIN PRESSURIZATION WITH NR 3 PACK. RETURNED TO FIELD FOR A SAFE LANDING. WHILE TROUBLESHOOTING, FOUND CONNECTOR FOR NR 1 PACK DIRTY, CLEANED AND REINSTALLED CONNECTOR IAW 747 MM 21-51-01 PAGE 401. OPS C
- [SDR WRNA20060031](https://openairdocs.org/sdr/WRNA20060031.md): Fire Loop · malfunctioned · Aug 1, 2006 · N923FT · Boeing 7472U3B · Extinguishing System
  > AFTER LANDING, ON TAXI IN, RECEIVED A FIRE WARNING FOR NR 4 ENGINE, A/C WAS STOPPED, ENGINE WAS SHUT DOWN AND FIRE HANDLE WAS PULLED. INDICATIONS OF FIRE CONTINUED, THE RIGHT ENGINE FIRE BOTTLE SWITCH WAS PUSHED, NO INDICATION OF DISCHARGE, THE LEFT FIRE BOT
- [SDR WRNA200600017](https://openairdocs.org/sdr/WRNA200600017.md): Diaphragm · failed · Jun 11, 2006 · N923FT · Boeing 7472U3B · Stabilizer Control System
  > AFTER TAKE OFF RUDDER RATIO LIGHT ILLUMINATED ABOVE 210 KNOTS, EXTINGUISHED BELOW 210 KNOTS RETURNED TO FIELD, A SAFE LANDING WAS MADE. FOUND PITOT LEAK IN LOWER RIGHT AUX PITOT SYSTEM CAUSED BY FAILED DIAPHRAGM IN RIGHT STABILIZER MODULE CONTROL PACKAGE, REP
- [SDR 200600296](https://openairdocs.org/sdr/200600296.md): Slide · no test · Apr 3, 2006 · N923FT · Boeing 7472U3B · Escape Slide
  > UPPER DECK CREW ESCAPE SLIDE RELEASED BUT SLIDE DID NOT DEPLOY DURING MAINTENANCE WHEN TRYING TO SHUT DOOR.
- [SDR 200600293](https://openairdocs.org/sdr/200600293.md): Bulkhead · corroded · Mar 7, 2006 · N923FT · Boeing 7472U3B · Fuselage Main, Bulkhead
  > BS 1480 FWD BULKHEAD WEB, LBL 36-42, LBL 51.5 AND RBL, 24.75, CORROSION - REPAIR. THIS ECRA PROVIDES INSTRUCTIONS TO REMOVE CORROSION, HFEC INSPECT TO VERIFY ALL DAMAGE IS REMOVED, SPOTFACE THE FASTENER LOCATIONS FOR PROPER SEATING OF THE FASTENERS, AND TO OV
- [SDR 200600294](https://openairdocs.org/sdr/200600294.md): Frame · corroded · Mar 7, 2006 · N923FT · Boeing 7472U3B · Fuselage Main, Frame
  > BS 2360 BULKHEAD LOWER AFT CHORD CORROSION. THIS PROVIDES INSTRUCTIONS TO REPAIR THE BS 2360 BULKHEAD LOWER AFT CHORD BY REMOVING THE CORROSION, TRIMMING OUT THE TOOLING MARK, HFEC INSPECTING TO CONFIRM CORROSION AND CRACK FREE, INSTALL REPAIR STRAPS TO RESTO
- [SDR WRNA20050029](https://openairdocs.org/sdr/WRNA20050029.md): Engine · malfunctioned · Dec 10, 2005 · N923FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > CLIMBING OUT THRU 16K FT, NR 2 ENGINE SHUTTERED, ACCOMPANIED BY LOUD NOISE. HIGH EGT, EPR AND OIL PRESSURE, TEMP ALL WITHIN LIMITS. SHUT DOWN NR 2 ENGINE. AIRCRAFT RETURNED TO FIELD, LANDING NORMAL.
- [SDR WRNA200500012](https://openairdocs.org/sdr/WRNA200500012.md): Actuator · unserviceable · Apr 28, 2005 · N923FT · Boeing 7472U3B · Rudder Control System
  > RUDDER RATIO LIGHT ILLUMINATED WHILE ACCELERATING TO 230KTS IND. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. REMOVED AND REPLACED LOWER RUDDER LINEAR ACTUATOR IAW 27-21-12. FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE.
- [SDR P5CA0401019](https://openairdocs.org/sdr/P5CA0401019.md): Duct · leaking · Dec 25, 2003 · N923FT · Boeing 7472U3B · Pneumatic Distribution System
  > BLEED AIR LEAK, APU SUPPLY DUCT AFT OF BULK CARGO COMPARTMENT. ITEM TRANSFERRED TO DMI 32017 AND MEL 49-01-01 PER DDPG.
- [SDR P5CA0301010](https://openairdocs.org/sdr/P5CA0301010.md): Fcu · failed · Dec 21, 2003 · N923FT · Boeing 7472U3B · Fuel Controlling System
  > NR 3 ENG WOULD NOT START, NO FUEL FLOW. CHECKED FUEL CONDITION MOTOR OPS NRML S/OFF VALVE ON FRONT SPAR CHECKED NORMAL. PERFORMED FUEL PUMP PRESS TEST ON FP 12 PORT, CHECKED GOOD. BLED FUEL LINES ON FUEL CONTROL UNIT, ENGINE RAN UP OK 71-00-00.
- [SDR P5CA0301008](https://openairdocs.org/sdr/P5CA0301008.md): Valve · failed · Dec 20, 2003 · N923FT · Boeing 7472U3B · Fuel Heater
  > NR 1 ENG FUEL HEAT FAILED IN OPEN POS WITH ICING LIGHT ON, FUEL TEMP MAX. PER FIM 73-01-00 PG 203 FOUND ZERO VOLTAGE AT SOCKETS BAND ON FUEL HEAT VLV CONNECTOR. REMOVED AND REPLACED FUEL HEAT VLV IAW MM 73-14-01, OPS NORMAL ON ENG RUN.
- [SDR P5CA0301007](https://openairdocs.org/sdr/P5CA0301007.md): Control Unit · malfunctioned · Dec 16, 2003 · N923FT · Boeing 7472U3B · Trailing Edge Flap Control System
  > AFTER T/O - INBOARD TRAILING EDGE FLAPS HUNG AT 5 DEGREES RETRACTED BY ALTS SYS ON EXTENSION I/B FLAPS HUNG AT 5 DEGREES EXTENDED BY ALT SYS. REPLACED NO COAST DRAG BRAKE PER MM 27-51-42, OP'S CK GOOD.
- [SDR P5CA0300986](https://openairdocs.org/sdr/P5CA0300986.md): Indicator · failed · Nov 14, 2003 · N923FT · Boeing 7472U3B · Engine Oil Pressure
  > ON ENGINE START NR 2 INDICATED NO OIL PRESS ON F/E PANEL OR FORWARD PANEL. REPLACED NR 2 ENGINE OIL PRESS INDICATOR SYSTEM CHECKS GOOD IAW MM 79-30-00.
- [SDR P5CA0300966](https://openairdocs.org/sdr/P5CA0300966.md): Indicator · fluctuates · Oct 14, 2003 · N923FT · Boeing 7472U3B · Airspeed/Mach Indicator
  > FIRST OFFICER'S BARBER POLE IN AIRSPEED INDICATOR FLUCTUATES, CAUSING MACH WARNING TO GO OFF. REPLACED A/S INDICATOR.
- [SDR P5CA0300967](https://openairdocs.org/sdr/P5CA0300967.md): Csd · malfunctioned · Oct 14, 2003 · N923FT · Boeing 7472U3B · Alternator-Generator Drive
  > ON TAXI, NOTED NR 2 & 4 GENERATOR SHOWED NO KW'S AND NO VOLTAGE FREQUENCY. ALSO, NR 3 CSD LIGHT ON FLIGHT ENGINEER'S PANEL - READ ANNUNCIATOR. SERVICED NR 2 & 4 CSD'S. RAN ENGINES AND DISCONNECTED NR 2 & 4 CSD'S. RECONNECTED NR 2 & 4 CSD'S. RE-RACKED GCU
- [SDR P5CA0300959](https://openairdocs.org/sdr/P5CA0300959.md): Rib · dented · Oct 4, 2003 · N923FT · Boeing 7472U3B · Horizontal Stabilizer, Spar/Rib
  > LT HORIZONTAL STABILIZER RIB CRACKED STABILIZER L/E STA 285 - 4 INCH CRACK. REMOVED LT HORIZONTAL STABILIZER DUE TO FOUND DENTED & REPAIRED RIB (4 INCH CRACK) AT LEADING EDGE STA 285.
- [SDR P5CA0300951](https://openairdocs.org/sdr/P5CA0300951.md): Control Quadrant · faulty · Sep 23, 2003 · N923FT · Boeing 7472U3B · Rudder Tab Control System
  > RUDDER RADIO LIGHT CAME ON WHEN FLAPS MOVING 5 TO 1 AT 220KNTS. REMOVED AND REPLACED RUDDER UPPER CONTROL IAW 27-21-13 LEAK CHECK GOOD.
- [SDR P5CA0300955](https://openairdocs.org/sdr/P5CA0300955.md): Push-Pull Cable · failed · Sep 22, 2003 · N923FT · Boeing 7472U3B · Engine Controls
  > NR 4 ENGINE THROTTLE BINDED NR 4 ENG FUEL CONDITION MOTOR POPPED C/B. REPLACED ENGINE PUSH PULL CABLE IAW MM 76-11-07 OPS CK OK. REPAIRED WIRE IAW STANDARD PRACTICES 20-00-00. OPS CK OK IAW AMM 76-11-00
- [SDR P5CA0300953](https://openairdocs.org/sdr/P5CA0300953.md): Actuator · defective · Sep 22, 2003 · N923FT · Boeing 7472U3B · Rudder Tab Control System
  > RUDDER RATIO LIGHT CAME ON AFTER FLAPS UP. REPLACED LOWER RUDDER RATIO CHANGER ACTUATOR IAW MM 27-21-12
- [SDR P5CA0300952](https://openairdocs.org/sdr/P5CA0300952.md): Actuator · defective · Sep 22, 2003 · N923FT · Boeing 7472U3B · Rudder Tab Control System
  > RUDDER RATIO LIGHT CAME ON AFTER FLAPS UP. REPLACED UPPER RUDDER RATIO CHANGER ACTUATOR AND ADJUSTED UPPER RUDDER IAW MM 27-21-12 AND 27-21-00.
- [SDR P5CA0300939](https://openairdocs.org/sdr/P5CA0300939.md): Wire · damaged · Sep 8, 2003 · N923FT · Boeing 7472U3B · Pneumatic System Wiring
  > RT WING LEADING EDGE OVERHEAT LIGHT ON WITH SMALL INCREASE OF PWR. FOUND DAMAGED WIRE AT SWITCH 1046 REPAIRED WIRE PER 20-50-2.
- [SDR P5CA0300940](https://openairdocs.org/sdr/P5CA0300940.md): Connector · disconnected · Sep 8, 2003 · N923FT · Boeing 7472U3B · Overheat Detection
  > AFT 20 MINUTES INTO CRUISE RT WING L/E OVERHEAT LIGHT ILLUMINATED. REMAINED ON UNTIL BLOCK IN. FOUND NR 3 PYLON DETECTOR S1046 SHORTED. DISCONNECTED S1046. ITEM DEFERRED PER MEL 26-22-03A. SECOND LOOP OPS NRML PER MM 26-15-00
- [SDR P5CA0300938](https://openairdocs.org/sdr/P5CA0300938.md): Duct · loose · Sep 7, 2003 · N923FT · Boeing 7472U3B · Pneumatic Distribution System
  > RT WING L/E OVERHEAT LIGHT CAME ON TAXI OUT. REMAINED ON WHEN ISOLATED. FOUND LOOSE DUCT LEADING TO NR 3 LEADING EDGE FLAP MOTOR. TIGHTENED AS REQUIRED SYS LEAK CK GOOD IAW MM 27-81-00 PG 207.
- [SDR P5CA0300925](https://openairdocs.org/sdr/P5CA0300925.md): Compressor · stalled · Aug 22, 2003 · N923FT · Boeing 7472U3B · Turbine Engine Compressor Section
  > ENGINE COMPRESSOR STALL ON DESCENT. REMOVED AND REPLACED NR 3 ENG, REF PAC ENG CHANGE WORK CARDS 7100-002.
- [SDR P5CA03000915](https://openairdocs.org/sdr/P5CA03000915.md): Fuel Control · overheated · Aug 17, 2003 · N923FT · Boeing 7472U3B · Fuel Control/Turbine Engines
  > ON DESCENT INTO HKG AT FL 360 NR 3 ENG FUEL TEMP WENT OFF SCALE HOT AND NR 3 ENG STALLED OUT. CORRECTIVE ACTION TAKEN: REPLACED NR 3 ENG FUEL CNTRL IAW AMM 73-21-01 LEAK CK OK PERFORMED TEST NR 9 FUEL CONTROL TRIM OK IAW 71-00-00 PG 580.
- [SDR P5CA03000316](https://openairdocs.org/sdr/P5CA03000316.md): Compressor · stalled · Aug 17, 2003 · N923FT · Boeing 7472U3B · Turbine Engine Compressor Section
  > NR 3 ENG COMPRESSOR STALLED AT FL 330 FUEL TEMP PEGGED AT OFF SCALE HOT AND OIL TEMP WENT TO 150 DRGS. PREFORMED 8TH STAGE BLEED CHECK VALVE. CHECKED P/R LINE ON T12 SENSOR, CHECKED FUEL HEAT VALVE, CHECKED NR 3 MAIN TANK SUMP DRAIN CHECKED FUEL / OIL COOLER
- [SDR P5CA0300914](https://openairdocs.org/sdr/P5CA0300914.md): Valve · malfunctioned · Aug 16, 2003 · N923FT · Boeing 7472U3B · Fuel Heater
  > PRIOR TO DESCENT APPLIED FUEL HEAT TO NR 3 ENG, FUEL HEAT DID COME DOWN AND PEGGED HOT ENG STALL ON DESCENT. PERFORMED A PRECAUTIONARY ENG SHUT DOWN AT 1600 FT ACCORDING TO PROCEDURE.
- [SDR P5CA0300911](https://openairdocs.org/sdr/P5CA0300911.md): Engine · power loss · Aug 11, 2003 · N923FT · Boeing 7472U3B · Engine (Turbine/Turboprop)
  > NR 3 ENG STALL CONDITION AFTER DESCENT FROM FL 330. PERFORMED FULL NR 3 ENG INSP. SUMPED ALL FUEL TANKS. CHECKED AND INSPECTED EVBC SCREEN. CHECKED FCU LINES FOR SECURITY AND NO LEAKAGE. PERFORMED ENG RUN ALL PARAMETERS IND NORMAL TO, OK TO CONTINUE SRVC. IAW
- [SDR P5CA0300910](https://openairdocs.org/sdr/P5CA0300910.md): Filter · contaminated · Aug 11, 2003 · N923FT · Boeing 7472U3B · Engine Fuel Distribution
  > ON DECENT NR 3 ENG HAD STALLED CONDITION. AT FL 290 SHUT DOWN. ON SECOND RESTART WITH FUEL HEAT APPLIED OPERATION NORMAL. CORRECTIVE ACTION TAKEN: REMOVED FUEL FILTER. INSPECTED AND CLEANED WATER FROM FILTER. REINSTALLED FILTER PERFORMED AURAL CK OF FUEL HEAT
- [SDR P5CA0300906](https://openairdocs.org/sdr/P5CA0300906.md): Cdu · malfunctioned · Aug 3, 2003 · N923FT · Boeing 7472U3B · Flight Management Computing Hardware System
  > NR 1 INS DISPLAY WENT BLANK AFTER PUSH BACK WARNING LIGHT CAME ON AND ADI TUMBLED. SWAPPED NR 1 CDU AND NR 3 CDU OPERATIONAL CHECK NORMAL PER MM 34-41-02.
- [SDR P5CA0300894](https://openairdocs.org/sdr/P5CA0300894.md): Connector · dirty · Jul 3, 2003 · N923FT · Boeing 7472U3B · Fuel Controlling System
  > NR 2 ENG WILL NOT START. NO FUEL FLOW. NR 2 ENG FUEL CONDITION ACTUATOR PLUG CLEANED AND RESECURED. ACTUATOR EXERCISED. ENG START SATIS. SUSPECT WIRING TO FUEL CONDITION ACTUATOR.
- [SDR P5CA0300895](https://openairdocs.org/sdr/P5CA0300895.md): Actuator · malfunctioned · Jul 3, 2003 · N923FT · Boeing 7472U3B · Fuel Controlling System
  > NR 2 ENGINE FAILED TO START (NO FUEL) AFTER SECOND ATTEMPT. PRESSURE CHECKED FUEL PUMP IAW MM 71-00-00. REMOVED FUEL CONDITION ACTUATOR CHECKED SHAFT. REINSTALLED FUEL CONDITION ACTUATOR ENG RUN/ OPS CK
- [SDR P5CA0300875](https://openairdocs.org/sdr/P5CA0300875.md): Warning Light · illuminated · May 4, 2003 · N923FT · Boeing 7472U3B · Hydraulic System, Main
  > NR 1 HYD SYS HEAT LIGHT ON. RAN AND CHECKED ENG & ADP'S OPERATING FLAPS TEMPS WERE SIMILAR & BELOW 100 C PER TEMP IND. DEFERRED O/TEMP LIGHT PER MEL 29-10.
- [SDR P5CA0300871](https://openairdocs.org/sdr/P5CA0300871.md): Blade · broken · Apr 25, 2003 · N923FT · Boeing 7472U3B · Windshield/Door Rain/Ice Removal
  > CAPT'S WIPER BLADE BROKE OFF DURING TAXI. INSP ARM AND DEFERRED ITEM PER DDPG - WAS LATER REPLACED IN PIK. BLADE SHEARED OFF ARM.
- [SDR P5CA0300781](https://openairdocs.org/sdr/P5CA0300781.md): Flap · failed · Mar 16, 2003 · N923FT · Boeing 7472U3B · Trailing Flap Position Indicating System
  > OUTBOUND FLAPS FAILED TO EXTEND PRIOR TO TAXI. FLAPS WERE CYCLED ELECTRICALLY & THEN WITH HYDRAULICS. OPS CHECK WAS SATISFACTORY. UNABLE TO DETERMINE THE CAUSE AT THE TIME.
- [SDR P5CA0300780](https://openairdocs.org/sdr/P5CA0300780.md): Connector · damaged · Mar 16, 2003 · N923FT · Boeing 7472U3B · Trailing Flap Position Indicating System
  > OUTBOUND FLAPS WOULD NOT EXTEND NORMALLY, HAD TO BE EXTENDED ELECTRICALLY. FOUND LOOSE PIN ON OUTBOARD RT POS TRANSMITTER CONNECTOR. REPINNED CONNECTOR & OPERATED FLAPS PER 27-51-00.
- [SDR P5CA0300769](https://openairdocs.org/sdr/P5CA0300769.md): Skin · dented · Feb 24, 2003 · N923FT · Boeing 7472U3B · Fuselage Main, Plate/Skin
  > DENT PUSHED INBD AT EXT FUSELAGE SKIN STA 400 LH - STR 27. DAMAGE AREA TRIMMED OUT. REINFORCED AREA W/ DOUBLER PER SRM 53-30-03, FIG. 1.
- [SDR P5CA0300768](https://openairdocs.org/sdr/P5CA0300768.md): Seat Track · corroded · Feb 24, 2003 · N923FT · Boeing 7472U3B · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND UPPER LOBE MAIN DECK SEAT TRACK LBL 1133, RT STA 1480-1660. DAMAGE SEAT TRACK PORTION REMOVED. NEW FABRICATE M/F 7075T6SM EXTRU BAC 1520-1889 PER DWG 866-17-19743-SH-2.
- [SDR P5CA0200705](https://openairdocs.org/sdr/P5CA0200705.md): Tire · out of balance · Oct 26, 2002 · N923FT · Boeing 7472U3B · Tire
  > ON TAKEOFF ROLL FROM RWY 24L-ANC, A VIBRATION BEGAN & INCREASED IN INTENSITY. AT 100 KTS IT BECAME VERY SEVERE. T/O WAS REJECTED AT 110 KTS. VIBRATION SEEMED MOST SEVERE IN NOSE GEAR REGION OR MAIN GEAR. DURING DECELERATION, A/C PULLED TO THE RIGHT. PERFO
- [SDR P5CA0200674](https://openairdocs.org/sdr/P5CA0200674.md): Indicator · faulty · May 13, 2002 · N923FT · Boeing 7472U3B · Engine Start Valves/Controls
  > NR 3 ENG START VALVE OPEN LIGHT CAME ON AFTER TAKEOFF AT 8,000 FT. SHUT DOWN NR 3 ENG, LIGHT WENT OUT AFTER SHUT DOWN AT APPROX 3,000 FT. TROUBLESHOT SYSTEM AND FOUND LIGHT INDICATION SYSTEM AT FAULT.
- [SDR P5CA0200671](https://openairdocs.org/sdr/P5CA0200671.md): Seal · burned · Apr 10, 2002 · N923FT · Boeing 7472U3B · Turbine Section
  > NR 4 ENGINE 1ST STAGE TURBINE OUTER AIR SEAL HAS 2 INCH BURN THROUGH. ENGINE TO BE REMOVED FROM SERVICE IN 60 HRS PER MM 72-00-00, PAGE 680N, TABLE 6.
- [SDR P5CA0200658](https://openairdocs.org/sdr/P5CA0200658.md): Screw · missing · Mar 6, 2002 · N923FT · Boeing 7472U3B · Leading Edge Slat Control System
  > L/H INBD L/E FLAPS ARE DEPLOYED BUT IND UP AT F/E'S PANEL & FWD IND. ON INSPECTION FOUND PDU DRIVE SHAFT DISCONNECTED, LOCKING SCREW MISSING & LOCKING SLEEVE MIGRATED FROM CONNECTION. RE-RIGGED & RE-ATTACHED DRIVE SHAFT IAW MM 27-81-02. OPS CHECK NORMAL.
- [SDR P5CA0200639](https://openairdocs.org/sdr/P5CA0200639.md): Latch · unlocked · Feb 3, 2002 · N923FT · Boeing 7472U3B · Cargo/Baggage Doors
  > AFTER TAKEOFF, MAIN DECK SIDE CARGO DOOR LIGHT ILLUMINATED. EMERGENCY DECLARED. 180,000 LBS OF FUEL WAS JETTISONED AND PRECAUTIONARY RETURN TO ICN WAS COMPLETED. WARNING LIGHTS REMAINED ILLUMINATED AT BLOCK IN. UPON INSPECTION, FOUND LATCH IN THE UNLOCKED
- [SDR P5CA0200626](https://openairdocs.org/sdr/P5CA0200626.md): Reducer · cracked · Jan 12, 2002 · N923FT · Boeing 7472U3B · Hydraulic System, Main
  > LOST ALL HYD ON NR 1 HYD SYS AFTER LANDING. FOUND RT TRUCK POSITIONER BYPASS REDUCER FLANGE CRACKED. REMOVED AND REPLACED ASSY PER MM 32-13-16, IPC 32-13-05-02 NR 40. BLED SYSTEM UNTIL NO AIR NOTED.
- [SDR P5CA0100611](https://openairdocs.org/sdr/P5CA0100611.md): Web · cracked · Nov 13, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, Structure
  > 1-1/2" CRACK BETWEEN STA 280 & 300 LH OB INTERCOSTAL ON NOSE WHEEL WELL ROOF RUNNING ACROSS UPPER FLANGE & DOWN THE WEB OF THE "Z" SECTION. NO ADJACENT FASTENERS ARE MISSING, LOOSE OR SHEARED. REPAIRED AS PER SRM 51-40-04, FIG 2, DETAIL 2.
- [SDR P5CA0100612](https://openairdocs.org/sdr/P5CA0100612.md): Web · cracked · Nov 13, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, Structure
  > 6" CRACK AT STA 300 RH NOSE WHEEL WELL BEAM RUNNING ACROSS WEB, EMINATING FROM INSULATION BLANKET STANDOFF HOLE. NO ADJACENT FASTENERS LOOSE, SHEARED OR MISSING. REPAIR CARRIED OUT IAW SRM 51-40-02, FIG 1, SHT 5, DETAIL 3. PARTS TREATED W/ ALODINE 1200 & REPAI
- [SDR P5CA0100603](https://openairdocs.org/sdr/P5CA0100603.md): Light · inoperative · Oct 21, 2001 · N923FT · Boeing 7472U3B · Emergency Lighting
  > UPPER DECK CENTER EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER MM 33-51-00.
- [SDR P5CA0100591](https://openairdocs.org/sdr/P5CA0100591.md): Warning System · malfunctioned · Sep 14, 2001 · N923FT · Boeing 7472U3B · Door Warning System
  > MAIN DECK SIDE CARGO DOOR WARNING LIGHT ILLUMINATED DURING ROTATION AT TAKEOFF. AIRCRAFT RETURNED TO AIRPORT. CYCLED DOOR OPEN AND INSPECTED LATCHES. DOOR CLOSED OK AND LOCKING LEVER CLOSED DOWN. OK FOR SERVICE PER MM 52-32-00.
- [SDR P5CA0100514](https://openairdocs.org/sdr/P5CA0100514.md): Balance Weight · corroded · Mar 28, 2001 · N923FT · Boeing 7472U3B · Rudder Structure
  > LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT SEVEN ON UPPER RUDDER. REPAIRED PER S/L 747-55-07.
- [SDR P5CA0100523](https://openairdocs.org/sdr/P5CA0100523.md): Balance Weight · corroded · Mar 26, 2001 · N923FT · Boeing 7472U3B · Rudder Structure
  > LEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE UPPER RUDDER. REPAIRED PER S/L 747-55-07.

Next page: https://openairdocs.org/deregistered/N923FT-2017-12-21/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 = 'N923FT' AND deregistration_id = 'N923FT-2017-12-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N923FT-2017-12-21/reports

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