# Service difficulty reports: Boeing 727-24C

A list on [Boeing 727-24C](https://openairdocs.org/model/boeing-727-24c.md).

Newest first. General aviation reporting is voluntary.

- [SDR 02FDEA00944](https://openairdocs.org/sdr/02FDEA00944.md): Downlock Switch · inoperative · Dec 13, 2002 · N114FE · Boeing 72724C · Landing Gear Position and Warning
  > DURING LANDING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. NO DOWN, GREEN LIGHT. NOTE: MANUAL GEAR EXTENSION PROCEDURE COMPLETED EMERGENCY, DECLARED WITH ATC. TROUBLESHOT LANDING GEAR POSITION INDICATING SYSTEM IAW M.M. FOUND FAULTY NOSE LANDING
- [SDR 01FDEA00125](https://openairdocs.org/sdr/01FDEA00125.md): Relief Valve · failed · Feb 15, 2001 · N114FE · Boeing 72724C · Turbine Engine Oil System
  > WHILE IN FLT NR 2 ENG OIL PRESSURE ABOVE RED LINE (60 PSI) COMPLIED WITH RED TABS TO SHUT DOWN ENG. NOTE: ABOVE RED LINE FOR LESS THAN 5 MIN WHILE ADDRESSING PROB. OIL TEMP CONT TO RISE AND WAS EVENTUALLY 120 DEG C. *S/D* REMOVED AND REPLACED NR 2 ENG OIL
- [SDR 00FDEA00012](https://openairdocs.org/sdr/00FDEA00012.md): Gearbox · leaking · Jan 13, 2000 · N114FE · Boeing 72724C · Turbine Engine Reduction Gear
  > 00-12 - 15 MIN IN CR FLT NR 2 ENG RAPIDLY LOST OIL QUANTITY WITH ENSUING OIL PRESS LOSS. RED TABS COMPLIED WITH AND NR 2 ENG SHUTDOWN, EMERGENCY DECLARED WITH A INFLT EMERG DIVERT TO IND.. REMOVED AND REPLACED NR 2 ENGINE GEAR BOX PER FEDEX ENGINE MAINTENANC
- [SDR 98FDEA00209](https://openairdocs.org/sdr/98FDEA00209.md): Duct · failed · Mar 20, 1998 · N114FE · Boeing 72724C · Pneumatic Distribution System
  > DURING CLIMBOUT, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. BOTH NR 3 BLEED AND RIGHT PACK WERE ON AT THE TIME. AFTER RED TABS CALLED FOR CLOSING/OFF ON BOTH NR 3 BLEED AND RIGHT PACK, THE NR 3 STRUT LIGHT WENT OUT. ENGINE PARAMETERS OK. REMOVED AND REPLA
- [SDR 98FDEA00208](https://openairdocs.org/sdr/98FDEA00208.md): Gasket · leaking · Mar 19, 1998 · N114FE · Boeing 72724C · Airfoil Anti/De-ice System
  > 98-0074, DURING CLIMB-OUT, THE NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. ENG NR 3 BLEED AIR SWITCH WAS CLOSED AT THE TIME THE LIGHT ILLUM. APPROPRIATE RED TABS WERE ACCOMPLISHED AND THE LIGHT WENT OUT PRIOR TO THE STEP REQUIRING POWER REDUCTION. WING ANTI-ICE WA
- [SDR 97FDEA00886](https://openairdocs.org/sdr/97FDEA00886.md): Actuator · malfunctioned · Dec 12, 1997 · N114FE · Boeing 72724C · Landing Gear Door Actuator
  > UPON GEAR EXTENSION RIGHT GEAR DOOR AND RED DOORS LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND ALL WAS NORMAL. OPERATIONAL CKS OK PER ADJUSTMENT TEST PER MAINTENANCE MANUAL 32-62-11. FOR PRECAUTION REPLACED RIGHT DOOR ACTUATOR PER MAINTENANCE MANUAL 32-32-
- [SDR 97FDEA00869](https://openairdocs.org/sdr/97FDEA00869.md): Switch · failed · Nov 26, 1997 · N114FE · Boeing 72724C · Landing Gear Position and Warning
  > DURING GEAR RETRACTION, EXPERIENCED A RIGHT MAIN GEAR DOOR ANNUNCIATOR LIGHT. COMPLETED THE GEAR UNSAFE AND OR DOORS LIGHT GEAR HANDLE UP CHECKLIST. AFTER CYCLING THE GEAR, DOOR ANNUNCIATOR LIGHT EXTINGUISHED. REMOVED AND REPLACED RIGHT LAND LANDING GEAR DO
- [SDR 97FDEA00809](https://openairdocs.org/sdr/97FDEA00809.md): Switches · moisture contam · Nov 7, 1997 · N144FE · Boeing 72724C · Landing Gear Position and Warning
  > RIGHT MAIN GEAR DOOR LIGHT ON SECOND OFFICER'S ANNUNCIATOR PANEL AND RED GEAR DOOR LIGHT ON GEAR POSITION PANEL REMAINED ILLUMINATED AFTER EXTENSION. GEAR INDICATION NORMAL AFTER RECYCLING. INSPECTED DOOR SWITCHES, FOUND SOME MOISTURE, CLEANED WITH CONTACT C
- [SDR 97FDEA00529](https://openairdocs.org/sdr/97FDEA00529.md): Frame · corroded · Aug 12, 1997 · N114FE · Boeing 72724C · Fuselage Main, Frame
  > NR 0380 - WHILE WORKING CARD NR 0142, FOUND CORROSION ON STA 1130 FRAME, LBL 25, WL 150 AT FASTENER HOLES. ACCOMPLISHED REPAIR TO BS 1130 FRAME AT LBL 25 PER FED-EX SRM 51-40-3.
- [SDR 97FDEA00528](https://openairdocs.org/sdr/97FDEA00528.md): Keel Beam · cracked · Aug 12, 1997 · N114FE · Boeing 72724C · Fuselage Main, Keel
  > NR 0054 IN THE AFT CARGO BAY, FOUND CRACK IN STR 29L KEEL BEAM AT BS 1082 AND CORROSION AT BS 1055. REMOVED AND REPLACED STRINGER 29L KEEL BEAM IAW FED-EX SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2, 53-30-3.
- [SDR 97FDEA00525](https://openairdocs.org/sdr/97FDEA00525.md): Flap · corroded · Aug 11, 1997 · N114FE · Boeing 72724C · Trailing Edge Flaps
  > LT WING I/B MIDFLAP T/E WEDGE UPPER IS CORRODED APPROX 18 INCHES AND 64 INCHES FROM O/B END. *S/D* REMOVED AND REPLACED WITH SERVICEABLE LT WING I/B MIDFLAP IAW FED-EX M/M 27-51-1. FUNCTIONAL TESTED GOOD IAW FED-EX M/M 27-51-1.
- [SDR 97FDEA00541](https://openairdocs.org/sdr/97FDEA00541.md): Floorbeam · corroded · Aug 7, 1997 · N114FE · Boeing 72724C · Fuselage Main, Floor Beam
  > NR 0107 001 STA-PAE - CORROSION ON BS 328 FLOORBEAM UPPER FLANGE LBL 47, WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-1, 53-10-8, 51-10-2, 51-30-2.
- [SDR 97FDEA00507](https://openairdocs.org/sdr/97FDEA00507.md): Floorbeam · corroded · Aug 7, 1997 · N114FE · Boeing 72724C · Fuselage Main, Floor Beam
  > NR 0107 001 STA-PAE - CORROSION ON BS 328 FLOORBEAM UPPER FLANGE, LBL 47, WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-1, 53-10-8, 51-10-2, 51-30-2.
- [SDR 97FDEA00477](https://openairdocs.org/sdr/97FDEA00477.md): Indication · malfunctioned · Jul 29, 1997 · N114FE · Boeing 72724C · Landing Gear Position and Warning
  > 97-0141 NOSE GEAR DID NOT INDICATE A GREEN DOWN SAFE LIGHT ON FIRST TRY. CYCLED GEAR AND GOT SAFE INDICATION.
- [SDR 97FDEA00463](https://openairdocs.org/sdr/97FDEA00463.md): Retract Mech · lack of lube · Jul 22, 1997 · N114FE · Boeing 72724C · Landing Gear Retraction/Extension System
  > NOSE GEAR DIDN'T COME DOWN UNTIL RECYCLED HANDLE. LUBRICATED NOSE LANDING GEAR DRAG BRACE KNUCKLE ASSEMBLY. ALSO, REPLACED AERODYNAMIC SEAL AT FORWARD EDGE OF NOSE LANDING GEAR DOORS ON ACCOUNT OF TORN AND BULGING SEGMENT OF SEAL INTERFERING WITH SMOOTH OPER
- [SDR 96FDEA01603](https://openairdocs.org/sdr/96FDEA01603.md): Supply Duct · blown · Oct 22, 1996 · N114FE · Boeing 72724C · Engine Start Valves/Controls
  > FIRE LIGHT AND BELL NR 3 ENGINE AFTER TAKEOFF AT 600 FEET ABOVE GROUND LEVEL. AFTER THROTTLE BROUGHT TO IDLE FIRE LIGHT WENT OUT. BOTH FIRE LOOPS TEST GOOD. LANDED WITHOUT FURTHER INCIDENT. FOUND START VALVE SUPPLY DUCT BLOWN. REPLACED DUCT NR 3 ENGINE.
- [SDR 95FDEA00165](https://openairdocs.org/sdr/95FDEA00165.md): Seal · cracked · Feb 18, 1995 · N114FE · Boeing 72724C · Passenger/Crew Doors
  > FWD ENTRY DIFFICULT TO CLOSE AND OPEN. UPON CLOSER INSP FOUND A CRACKED SEAL AROUND UPR ROLLER ASSY AT REAR. UNABLE TO CLOSE DOOR COMPLETELY. (UPR AND LWR AFT ROLLER AREAS CRACKED.) REPAIRED DAMAGED FRAME PER EA 7-5210-23817. FWD ENTRY DOOR INSTALLED AND

## 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 aircraft_model_key = '72724C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-24c/reports

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