# Service difficulty reports: N184FE, cancelled Oct 15, 2002

A list on [N184FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N184FE-2002-10-15.md).

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

- [SDR 99FDEA00034](https://openairdocs.org/sdr/99FDEA00034.md): Landing Gear · vibrated · Jan 30, 1999 · N184FE · Boeing 72722 · Nose/Tail Landing Gear
  > VIBRATION IN THE AREA OF NOSE WHEEL AND A FLICKER OF A RED DOOR LIGHT ABOVE GEAR HANDLE. WHEN GEAR LEVER WAS RAISED NO ADDITIONAL VIB WERE FELT. INSPECTED NOSE GEAR WHEEL WELL DOOR CABLES AS PER MM 32-22-21 PG 601. NO DEFECTS FOUND. OK FOR SERVICE.
- [SDR 98FDEA00451](https://openairdocs.org/sdr/98FDEA00451.md): Switch · malfunctioned · Jul 11, 1998 · N184FE · Boeing 72722 · Landing Gear Position and Warning
  > 98-0176 STA-MEM: AFTER TAKEOFF WHEN GEAR WAS RAISED, THE GREEN NLG LIGHT AND RED GEAR DOOR LIGHT FOR NOSE GEAR REMAINED ON. AFM PROCEDURES WERE FOLLOWED BUT NO LUCK. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX AND NLG LOCK SWITCH PER M/M 32-61-21. RE
- [SDR 98FDEA00448](https://openairdocs.org/sdr/98FDEA00448.md): Switch · inop · Jul 9, 1998 · N184FE · Boeing 72722 · Landing Gear Position and Warning
  > STA-MEM: NOSE GEAR UNSAFE. RECYCLED 4 TIMES, FOURTH TIME AFTER 3 MINUTES DELAY GOT GREEN LIGHT. NOSE ALIGNMENT STRIPE SAFE. REPEAT. INSTALLED (3) GEAR LOCK PINS. REMOVED AND REPLACED NOSE GEAR POSITION SWITCH PER 32-61-20. OPERATIONAL CHECK PER MAINTENA
- [SDR 98FDEA00350](https://openairdocs.org/sdr/98FDEA00350.md): Retract Mech · lack of lube · May 15, 1998 · N184FE · Boeing 72722 · Landing Gear Retraction/Extension System
  > ON FINAL, NOSE GEAR DID NOT INDICATE DOWN (NO GREEN LIGHT) WHEN GEAR DOWN WAS INITIALLY SELECTED. GEAR HANDLE RECYCLED AND ALL GEAR INDICATED NORMAL DOWN AND LOCKED. LUBED NOSE GEAR, CYCLED GEAR SEVERAL TIMES, OPS CK NORMAL, INDICATED THREE GREEN LIGHTS, PER
- [SDR 97FDEA00849](https://openairdocs.org/sdr/97FDEA00849.md): Panel · malfunction · Nov 20, 1997 · N184FE · Boeing 72722 · Landing Gear Position and Warning
  > 97-0237 NOSE GEAR DID NOT INDICATE DOWN SAFE (GREEN LIGHT NOT ON.) NOSE GEAR LIGHT WOULD NOT TEST. GEAR DOOR LIGHT TRANSITIONED NORMALLY WITH EXTENSION AND RETRACTION. RED UNSAFE NOSE LIGHT TRANSITIONED NORMALLY AS WELL. FOUND LANDING GEAR/DOOR ANNUNCIATOR
- [SDR 97FDEA00806](https://openairdocs.org/sdr/97FDEA00806.md): Keel Beam · corroded · Nov 4, 1997 · N184FE · Boeing 72722 · Fuselage Main, Keel
  > NR 0388 016 CORROSION ON THE L/H KEEL BEAM BETWEEN SKIN BS 1065. *** S/D *** REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED PORTION BS 1057 TO 1087. REMOVED DAMAGED SKIN BS 1065. REMOVED DAMAGED SHEAR TIE. FABRICATED REPAIR PARTS. INST
- [SDR 97FDEA00801](https://openairdocs.org/sdr/97FDEA00801.md): Shear Tie · corroded · Nov 3, 1997 · N184FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0446 014 CORROSION (C53-113-01(2)) IN THE SHEAR TIE BS 990, BETWEEN STRINGERS 29 & 30 R/H. *** S/D *** REPAIRED SHEAR TIE AT BS 990, RBL 6, WL 151 IAW FED-EX SRM 53-10-4.
- [SDR 97FDEA00800](https://openairdocs.org/sdr/97FDEA00800.md): Splice · corroded · Nov 3, 1997 · N184FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0421 015 CORROSION IN THE STRINGER SPLICE AT BS 1057, STR 28 R/H. *** S/D *** REMOVED STRINGER SPLICE AT BS 1057. REMOVED STRINGER END PIECE AT BS 1040-1057. FABRICATED STRINGER END BS 1040-1057 AND INSTALLED WITH STR SPLICE AT BS 1057. IAW FE
- [SDR 7FDEA00791](https://openairdocs.org/sdr/7FDEA00791.md): Shear Tie · cracked · Oct 29, 1997 · N184FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0427 013 CORROSION (C53-113-01(2)) ON THE SHEAR TIE AT BS 1130 OUTBOARD OF STRINGER 29L. *** S/D *** REMOVED SHEAR TIE. FABRICATED NEW SHEAR TIE. INSTALLED PER FED-EX SRM 51-30-2. ALODINED, PRIMED AND PAINTED PER FED-EX SRM 51-10-2 AND PER FED
- [SDR 97FDEA00784](https://openairdocs.org/sdr/97FDEA00784.md): Floorbeam · corroded · Oct 28, 1997 · N184FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 0253 009 CORROSION (C53-224-06) ON FLOORBEAM BS 344, RBL 15-LBL 60, WL 208. UPPER CHORD OF 344 FLOORBEAM, RBL 65 TO LBL 65, WL 208 WAS FOUND TO BE OUT OF LIMITS. REMOVED CORRODED UPPER CHORD FROM RBL 65 TO LBL 65 AND INSTALLED NEW UPPER CHORD PER FED-EX D
- [SDR 97FDEA00783](https://openairdocs.org/sdr/97FDEA00783.md): Frame · cracked · Oct 28, 1997 · N184FE · Boeing 72722 · Fuselage Main, Frame
  > NR 0412 010 AFT CARGO BAY AT BS 1130, STR 26L THE FRAME IS CRACKED IN THE J SECTION. *** S/D ***INSTALLED DOUBLER ON FRAME AT 26L BS 1130 AFT CARGO BAY AS PER FED-EX SRM 51-40-3.
- [SDR 97FDEA00782](https://openairdocs.org/sdr/97FDEA00782.md): Rib · corroded · Oct 28, 1997 · N184FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0083 011 NR 2 K-FLAP CORRODED AT I/B BONDING JUMPER TO BULLNOSE. REMOVED CORROSION ON NR 2 K-FLAP I/B BULLNOSE ATTACH (LOWER) POINT FLANGE THICKNESS.140. REMOVED.030 WITHIN LIMTS PER FED-EX DWG NR SR 27-57-010. UPPER ATTACH POINT OUT OF LIMITS. INSTAL
- [SDR 97FDEA00781](https://openairdocs.org/sdr/97FDEA00781.md): Rib · corroded · Oct 28, 1997 · N184FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0173 012 CORROSION AT BONDING WIRE UPPER AND LOWER ATTACH POINTS ON NR 4 K-FLAP BULLNOSE, O/B END. REMOVED CORROSION AT BONDING WIRE UPPER AND LOWER ATTACH POINTS ON NR 4 K-FLAP BULLNOSE O/B END IAW FED-EX DRWG SR 27-57-010 REV C AND FED-EX SRM 57-50-3. U
- [SDR 97FDEA00777](https://openairdocs.org/sdr/97FDEA00777.md): Floorbeam · corroded · Oct 27, 1997 · N184FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 0103 008 CORROSION (C53-224-06) ON FLOORBEAM BS 328, LBL 37, WL 208. REMOVED CORROSION (C53-224-06) FOUND TO BE OUT OF LIMITS. REPAIRED BS 328, LBL 37, WL 208 PER FED-EX EA NR 7-5310-36824.
- [SDR 97FDEA00776](https://openairdocs.org/sdr/97FDEA00776.md): Stringer · cracked · Oct 27, 1997 · N184FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > NR 0417 007 AFT CARGO BAY AT BS 1113, STRINGER 28 R/H IS CRACKED ON INBOARD SIDE. *** S/D *** REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND PAINTED REPAIR PARTS. INSTALLED REPAIR PARTS FROM BS 1113 TO 1140, STR 20R. ALL IAW
- [SDR 97FDEA00771](https://openairdocs.org/sdr/97FDEA00771.md): Stringer · corroded · Oct 23, 1997 · N184FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-113-01, 2) ON INBOARD SIDE OF STRINGER 28 RT, BS 1130. *S/D* REMOVED AND REPLACED STRINGER 28 RT IAW FED-EX SRM 53-10-3 FIG 1 SHT 1 WORK ACCOMPLISHED ON NR0417.
- [SDR 97FDEA00768](https://openairdocs.org/sdr/97FDEA00768.md): Spar Chord · corroded · Oct 21, 1997 · N184FE · Boeing 72722 · Wing Spar
  > CORROSION (C53-224-05) WING CENTER SECTION FRONT SPAR LOWER CHORD RBL 25, BS 740. *S/D* FOUND CORROSION OUT OF LIMITS. REMOVED WING CENTER SECTION FRONT SPAR LOWER CHORD. INSTALLED NEW CHORD IAW FED-EX EA- 7-5710-36858.
- [SDR 97FDEA00761](https://openairdocs.org/sdr/97FDEA00761.md): Wedge · delaminated · Oct 17, 1997 · N184FE · Boeing 72722 · Leading Edge Devices
  > RT WING O/B MIDFLAP T/E WEDGE IS DELAMINATED 24 FROM I/B END AND AT THE NR 2 AFT FLAP TRACK, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.
- [SDR 97FDEA00760](https://openairdocs.org/sdr/97FDEA00760.md): Wedge · delaminated · Oct 17, 1997 · N184FE · Boeing 72722 · Leading Edge Devices
  > LT WING I/B MIDFLAP T/E WEDGE IS DELAMINATED AT 20 FROM I/B END, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.
- [SDR 97FDEA00755](https://openairdocs.org/sdr/97FDEA00755.md): Bonding Jumper · corroded · Oct 16, 1997 · N184FE · Boeing 72722 · Leading Edge Devices
  > NR 2 K-FLAP BULLNOSE CORRODED ON O/B BONDING JUMPER. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP O/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT IAW FED-EX SRM 57-50-3.
- [SDR 97FDEA00742](https://openairdocs.org/sdr/97FDEA00742.md): Wedge · delaminated · Oct 15, 1997 · N184FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0079 001, R/W I/B MIDFLAP T/E WEDGE IS DELAMINATED 16 FROM I/B END.

## 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 = 'N184FE' AND deregistration_id = 'N184FE-2002-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N184FE-2002-10-15/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.