# Service difficulty reports: N112FE, cancelled Aug 22, 2003

A list on [N112FE, cancelled Aug 22, 2003](https://openairdocs.org/deregistered/N112FE-2003-08-22.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 01FDEA00349](https://openairdocs.org/sdr/01FDEA00349.md): Switch · inoperative · May 15, 2001 · N112FE · Boeing 72722C · Leading Edge Slat Control System
  > 01-155 ON DEPART WHEN FLAP 2 DEG SEL ON RETRACTION LIGHT ON FWD PNL FLAP/SLAT IND REMAIN AMBER. FND L/E FLAP OVERRIDE TEST SWITCH IN OVERRIDE POS, RETURN TO NORM POSITION, OPS CK GOOD PER 727 MM 27-81-000-6.
- [SDR 00FDEA00838](https://openairdocs.org/sdr/00FDEA00838.md): Downlock Switch · failed · Dec 2, 2000 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 00-333 NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE WHEN MAINS CAME DOWN. R&R NOSE GEAR DOWN LOCK SWITCH PER MM 32-61-21. REMOVED GEAR PIN FOR FLIGHT. OPS CK NORMAL.
- [SDR 00FDEA00157](https://openairdocs.org/sdr/00FDEA00157.md): Valve · failed · Mar 15, 2000 · N112FE · Boeing 72722C · Fuel Heater
  > 00-87 - FUEL HEAT VALVE FAIL NR 1 ENGINE THEN OIL TEMP YELLOW ARC UNDER 15 MIN. REMOVED AND REPLACED VALVE PER 73-14-011-4. OPERATIONAL NORMAL.
- [SDR 00FDEA00032](https://openairdocs.org/sdr/00FDEA00032.md): Light · malfunctioned · Jan 25, 2000 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 00-19 - AFT RAISING LG 2 MIN WITH GEAR HANDLE OFF POS THE LMG DOOR LIGHT ILLUM. REMOVED AND REPLACED LMLG DOOR ACTUATOR PER MM 32-32-081. PERF GEAR EXT AND RETRACTION SEV TIMES. OPER CK NORMAL. AC OK TO CONTINUE SERVICE.
- [SDR 99FDEA00330](https://openairdocs.org/sdr/99FDEA00330.md): Accessory Unit · inop · Aug 12, 1999 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > RETRACTION REPEAT GEAR WARN LIGHT PROBLEMS. SYMPTOMS INDENTICAL TO ARD REPORT ON 8/11/99. REMOVED AND REPLACED LAND GEAR ASSY UNIT PER MM 32-09-111-5 PG 1-5 GROUND TEST GOOD. REMOVED AND REPLACED ANNUNCIATOR PANEL PER MM 32-62-001-4.
- [SDR 99FDEA00327](https://openairdocs.org/sdr/99FDEA00327.md): Accessory Unit · inop · Aug 11, 1999 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 99-203 REPEAT, 3 GEAR RED INTRANSIT LIGHTS WOULD NOT EXTINGUISH AFT RAISING GEAR HANDLE TO UP FLT ENGINE DOOR ANNUNCIATOR PNL NORM. REMOVED AND REPLACED LANDING GEAR ELECTRICAL MODULE PER MM 32-09-111-4 TEST PER MM 32-09-111-5. OPS CK GOOD.
- [SDR 99FDEA00325](https://openairdocs.org/sdr/99FDEA00325.md): Accessory Unit · inop · Aug 11, 1999 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 99-201 - AFT RAISING LAND GEAR HANDLE ALL 3 UNSAFE RED LIGHTS REMAIN ON. RERACKED LAND GEAR ACCESSORY UNIT, CYCLED LT MLG DOWNLOCK SWITCH, OPS CK NORM PER 727-100 M/M 32-62-001-4.
- [SDR 99FDEA00289](https://openairdocs.org/sdr/99FDEA00289.md): Switch · failed · Jul 28, 1999 · N112FE · Boeing 72722C · Engine Oil Indicating System
  > 99-174 - NR 3 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. ENG SHUTDOWN ACCOMPLISHED. REPLACED NR 3 ENG OIL FILTER BYPASS SWITCH PER MM 79-33-000-0. REPLACED MAIN OIL STRAINER FILTER. PERF ENG WINDMILLING TEST PER MM 72-00 PG 5100. OPS CK GOOD.
- [SDR 98FDEA00694](https://openairdocs.org/sdr/98FDEA00694.md): C1 Disk · bird strike · Nov 10, 1998 · N112FE · Boeing 72722C · Turbine Engine Compressor Section
  > AFT V1 AND BEFORE ROTATION NR 1 ENG GAVE A LOUD BANG AND APPEARED TO COMPRESSOR STALL, FOLLOWED BY A SMELL COMING FROM THE PACK A/C LEFT HAND. IN WORK AT THIS TIME TO REPLACE C1 DISK ASSY (BIRD INJESTION FOD). REMOVED AND REPLACED NR 1 ENG C1 DISK ASSY BREAT
- [SDR 98FDEA00669](https://openairdocs.org/sdr/98FDEA00669.md): Accessory Unit · malfunctioned · Oct 23, 1998 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 98-258 - AFTER GEAR HANDLE RAISED UP RIGHT MAIN GEAR INDICATED DOWN AND LOCKED. REMOVED AND REPLACED LAND GEAR ANNUNCIATOR PANEL DUE TO POSS OF PWR MM 33-10-00. REMOVED AND REPLACED LANDING GEAR ACCY UNIT. CYCLED GEAR SEVERAL TIMES AND ALL IND OPERATE NORM.
- [SDR 98FDEA00667](https://openairdocs.org/sdr/98FDEA00667.md): Prox Unit · inop · Oct 22, 1998 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 98-25 - WHEN GEAR HANDLE RAISED, RT MAIN GEAR IND DOWN (GREEN LIGHT) AND RED TRANSIT LIGHT WAS ILLUM. RECYCLED GEAR IN ACCORD WITH EMER PROC, NO HELP. RETURN TO GFK. AFTER RAISING GEAR AND PUT HANDLE TO OFF POS RED LIGHT OUT AND RIGHT MAIN GREEN LIGHT ILLUM
- [SDR 97FDEA00699](https://openairdocs.org/sdr/97FDEA00699.md): Downlock Switch · failed · Oct 2, 1997 · N112FE · Boeing 72722C · Landing Gear Position and Warning
  > 97-0193 ON FINAL APPROACH, NOSE GEAR LIGHT WAS ON, WENT OUT WITH FLAPS 30. (GOT WARNING HORN), AND THEN CAME BACK ON GREEN. WENT AROUND, CYCLED GEAR, CHECKED SAFE. INSPECTED NOSE GEAR SWITCHES AND MECHANISM, ALL CHECKS SATISFACTORY. REMOVED AND REPLACED NOS
- [SDR 97FDEA00443](https://openairdocs.org/sdr/97FDEA00443.md): Engine · malfunctioned · Jul 17, 1997 · N112FE · Boeing 72722C · Engine (Turbine/Turboprop)
  > 97-0134 AT T/O CREW FELT SLIGHT YAW AND OBSERVED NR 1 EPR DROP TO 1.4 ALL OTHER ENG IND REMAIN WITHIN LIMITS ALTHOUGH EGT WAS HIGHER THAN NORM. ENG WAS NEVER SHUTDOWN UNTIL SAFE LANDING WAS ACCOMP. SWAP NR 2 ENG PRESS BLEED CTRL AND BLEED CTRL VLV ON NR 1 EN
- [SDR 95FDEA01807](https://openairdocs.org/sdr/95FDEA01807.md): Fitting · cracked · Nov 27, 1995 · N112FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > BS 870 LT TERMINAL FITTING LOWER HOLE NR 4 SHOWS CRACK WITH A HFEC AT STR 9 TO 10. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND DOUBLER IAW 727-53-0194 BOEING SB AND INSTALLED ON A/C PER BOEING SB 727-53-0194.
- [SDR 95FDEA01806](https://openairdocs.org/sdr/95FDEA01806.md): Floorbeam · corroded · Nov 27, 1995 · N112FE · Boeing 72722C · Fuselage Main, Floor Beam
  > HEAVY CORROSION ON FLOORBEAM STA 560 LBL 0 TO 22. REMOVED CORROSION, FABRICATED REPAIR PIECES IAW 53-10-8, INSTALLED REPAIR PIECES, DOUBLER AND FASTENERS PER 53-10-8.
- [SDR 95FDEA01805](https://openairdocs.org/sdr/95FDEA01805.md): Floorbeam · corroded · Nov 27, 1995 · N112FE · Boeing 72722C · Fuselage Main, Floor Beam
  > STA 600 RBL 60 TO 41 WL 208.1 FLOORBEAM HAS CORROSION ON UPPER AND LWR LANDING. REMOVED TOP FLANGE OF FLOORBEAM RBL 44 TO 56 PER SRM 53-10-8 FIG 5 AND FABRICATED REPAIR AND INSTALLED PER SRM 53-10-8 FIG 5, 51-10-6 AND 51-10-1.
- [SDR 95FDEA01804](https://openairdocs.org/sdr/95FDEA01804.md): Clip · corroded · Nov 27, 1995 · N112FE · Boeing 72722C · Wing Miscellaneous Structure
  > WING TEE CLIP STA 760 RBL 665 HAS CORROSION. REMOVED CORRODED TEE CLIP, COLD WORKED HOLES PER EO 7-5710-7-2308 AND INSTALLED TEE CLIP.
- [SDR 95FDEA01803](https://openairdocs.org/sdr/95FDEA01803.md): Floorbeam · corroded · Nov 27, 1995 · N112FE · Boeing 72722C · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CORROSION STA 680 LBL 50 TO 55. CUT AWAY CORRODED AREA FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.
- [SDR 95FDEA01809](https://openairdocs.org/sdr/95FDEA01809.md): Fitting · cracked · Nov 26, 1995 · N112FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > SEVERAL STR END FITTINGS AT STA 870 AND 740 CRACKED ON INNER LANDING STR 8R AND L MPN'S 69-16380-3 AND 69-34593-1. REMOVED AND REPLACED END FITTINGS PER STANDARD PRACTICE.
- [SDR 95FDEA01808](https://openairdocs.org/sdr/95FDEA01808.md): Frame · cracked · Nov 26, 1995 · N112FE · Boeing 72722C · Fuselage Main, Frame
  > BS 804.5 LT SIDE 23 ABOVE WL 208.1 STR 14 FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 51-40-3.
- [SDR 95FDEA01699](https://openairdocs.org/sdr/95FDEA01699.md): Fittings · cracked · Nov 8, 1995 · N112FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > SEVERAL STRINGER END FITTINGS AT STA 870 TO 740 CRACKED ON INNER LANDING STR 8 RT AND LT MPN'S 69-16380-3 AND 69-34593-1.
- [SDR 95FDEA01693](https://openairdocs.org/sdr/95FDEA01693.md): Floorbeam · corroded · Nov 7, 1995 · N112FE · Boeing 72722C · Fuselage Main, Floor Beam
  > FLOORBEAM STA 640 LBL 53 HAS CORROSION.
- [SDR 95FDEA01692](https://openairdocs.org/sdr/95FDEA01692.md): Floorbeam · corroded · Nov 7, 1995 · N112FE · Boeing 72722C · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM STA 640 RBL 21 TO 58.
- [SDR 95FDEA01691](https://openairdocs.org/sdr/95FDEA01691.md): Floorbeam · corroded · Nov 7, 1995 · N112FE · Boeing 72722C · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CORROSION STA 680 LBL 50 TO 55.
- [SDR 95FDEA01690](https://openairdocs.org/sdr/95FDEA01690.md): Clip · corroded · Nov 7, 1995 · N112FE · Boeing 72722C · Wing Miscellaneous Structure
  > WING TOE CLIP STA 760 LBL 65 HAS CORROSION.

## 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 = 'N112FE' AND deregistration_id = 'N112FE-2003-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N112FE-2003-08-22/reports

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