# Service difficulty reports: N199FE, cancelled Aug 16, 2004

A list on [N199FE, cancelled Aug 16, 2004](https://openairdocs.org/deregistered/N199FE-2004-08-16.md).

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

- [SDR 03FDEA00179](https://openairdocs.org/sdr/03FDEA00179.md): Switch · failed · Feb 26, 2003 · N199FE · Boeing 727173C · Landing Gear Position and Warning
  > RED RT GEAR DOOR LIGHT ILLUMINATED ON LANDING GEAR RETRACTION. CREW CYCLED GEAR IAW QRH, LIGHT REMAINED ILLUMINATED FOR DURATION OF FLIGHT. REMOVED AND REPLACED RT MLG DOOR WARNING SWITCH IAW M/M 32-62-011-4 OPERATIONAL CHECK NORMAL.
- [SDR 02FDEA00182](https://openairdocs.org/sdr/02FDEA00182.md): Indicator · faulty · Mar 5, 2002 · N199FE · Boeing 727173C · Cabin Pressure Indicator
  > A/C W/N PRESSURIZE, APPEARED LEFT PACK NOT SUPPLYING AIR TO A/C. RAN ENGS, PERFORMED AIR COND AND PRESSURIZATION OPS TEST PER JET RUN HDBK CHAPTER 7 & 5A. PRESSURIZED IN AUTO AND MANUAL MODE. BOTH TEST CHECK NORM BOTH PACKS MAINTAIN AIR.
- [SDR 01FDEA00909](https://openairdocs.org/sdr/01FDEA00909.md): Warning System · malfunctioned · Oct 23, 2001 · N199FE · Boeing 727173C · Leading Edge Slat Position Indicating System
  > LEADING EDGE NR 6 FAILED DURING FLAP RETRACTION. OPERATED FLAPS & SLATS, ALL IND NORMAL PER MM 27-81-000-0.
- [SDR 00FDEA00122](https://openairdocs.org/sdr/00FDEA00122.md): Warning Light · illuminated · Mar 1, 2000 · N199FE · Boeing 727173C · Door Warning System
  > MAIN CARGO DOOR LIGHT ON AFT T/O.
- [SDR 96FDEA01682](https://openairdocs.org/sdr/96FDEA01682.md): Downlock Switch · malfunctioned · Nov 19, 1996 · N199FE · Boeing 727173C · Landing Gear Position and Warning
  > ON INITIAL LANDING GEAR EXTENSION THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. A VISUAL SCAN OF THE ALIGNMENT MARKS INDICATED THAT THE GEAR WAS DOWN. RECYCLED GEAR AS PER NOSE EXTENSION FAILURE PROCEDURES AND THE NOSE GEAR GREEN LIGHT ILLUMINATED NORMALLY.
- [SDR 96FDEA01331](https://openairdocs.org/sdr/96FDEA01331.md): Door · missing · Aug 7, 1996 · N199FE · Boeing 727173C · Landing Gear Doors
  > RAISED GEAR HANDLE AND HEARD LOUD BANG. FELT VIBRATIONS AND NOSE GEAR LIGHT REMAINED ILLUMINATED. LOWERED GEAR, DUMPED FUEL, AND RETURNED TO BASE. ****S/D***** LEFT FORWARD NOSE GEAR DOOR WAS FOUND TO BE MISSING. REPLACED LEFT FORWARD NOSE GEAR DOOR
- [SDR 96FDEA01285](https://openairdocs.org/sdr/96FDEA01285.md): Bear Strap · corrosion · Jul 24, 1996 · N199FE · Boeing 727173C · Fuselage Miscellaneous Structure
  > NR 0540 019. CORROSION C53-113-01(2). FOUND ON BEAR STRAP AND STAINLESS STEEL DOUBLER FROM BS 1075 - 1160, STR 225R WL 148.5. ****S/D***** COMING.
- [SDR 96FDEA01274](https://openairdocs.org/sdr/96FDEA01274.md): Skin · delaminated · Jul 21, 1996 · N199FE · Boeing 727173C · Fuselage Main, Plate/Skin
  > DISCREPANCY: (NR 0132) (18) SKIN DOUBLER IS DELAMINATED AT BS 1156, RBL 31, WL 158, BETWEEN STR 25R AND STR 26R. CORRECTIVE ACTION: REMOVED AND REPLACED SKIN PANEL IAW FEDEX EA 7-5330-29608.
- [SDR 96FDEA01249](https://openairdocs.org/sdr/96FDEA01249.md): Skin · corrosion · Jul 12, 1996 · N199FE · Boeing 727173C · Wing, Plate/Skin
  > DISCREPANCY: NR 0593 (017) FRETTING CORROSION AT FUEL CELL CUTOUT 7604 RT WING. CORRECTIVE ACTION: REPAIRED PER FEDEX EA 7-5710-29614. ALSO, CHANGED MODEL FROM 7272D4 TO 727173C AND S/N FROM 21849 TO 19509.
- [SDR 96FDEA01230](https://openairdocs.org/sdr/96FDEA01230.md): Rib · corroded · Jul 10, 1996 · N199FE · Boeing 727173C · Fuselage Miscellaneous Structure
  > NR 0479, 016, CRACK ON LT INTERNAL RIB STR 13 AFT SIDE OF BS 870 TERMINAL FITTING AREA, APPROX 4 INCHES IN LENGTH. *S/D* REPAIRED CRACK ON LT INTERNAL RIB STR 13 AFT SIDE OF BS 870 TERMINAL FITTING IAW FED EX EA 7-53-10-29173.
- [SDR 96FDEA01190](https://openairdocs.org/sdr/96FDEA01190.md): Skin · no edge distance · Jul 3, 1996 · N199FE · Boeing 727173C · Fuselage Main, Plate/Skin
  > NR0548 AND 015, SKIN HAS INSUFFICIENT EDGE DISTANCE AT BS 358 TO 360 AT STR 27L EXTERNAL SIDE OF SKIN.
- [SDR 96FDEA01189](https://openairdocs.org/sdr/96FDEA01189.md): Stringer · cracked · Jul 2, 1996 · N199FE · Boeing 727173C · Fuselage Main, Longeron/Stringer
  > NR0557 AND 014, WHILE WORKING NR0540, FOUND STR 28R AT BS 1057 TO BE CRACKED AND CORRODED. *S/D* REMOVED DAMAGE STRINGER SECTION AT BS 1057 AND INSTALLED REPAIRED PER SRM 53-10-3.
- [SDR 96FDEA01187](https://openairdocs.org/sdr/96FDEA01187.md): Fitting · cracked · Jul 1, 1996 · N199FE · Boeing 727173C · Fuselage Miscellaneous Structure
  > NR0019 AND 013, FOUND CRACKS IN STA 740 FORGING RT BETWEEN STR 18 TO 20 RT, FWD BAY. *S/D* REPAIRED CRACKS IN STA 740 FORGING RT BETWEEN STR 18 TO 20 RT IAW FEDEX EA 7-5310-29123.
- [SDR 96FDEA01186](https://openairdocs.org/sdr/96FDEA01186.md): Shear Tie · damaged · Jun 29, 1996 · N199FE · Boeing 727173C · Fuselage Miscellaneous Structure
  > NR0526 AND 012, SHEAR TIE DAMAGED AT BS 1148 BETWEEN STA 19 TO 20 RT ON FWD SIDE OF FRAME. *S/D* REPAIRED DAMAGED SHEAR TIE AT BS 1148 BETWEEN STR 19 AND 20 RT FWD SIDE OF FRAME IAW FEDEX SRM 53-10-4.
- [SDR 96FDEA01139](https://openairdocs.org/sdr/96FDEA01139.md): Frame · corroded · Jun 14, 1996 · N199FE · Boeing 727173C · Fuselage Main, Frame
  > NR 0546 AND 011. WHILE WORKING NR 0537, FOUND CORROSION ON FRAME BS 1110, WL 150, RBL 29 - RBL 34. BLENDED CORROSION, FOUND TO BE WITHIN LIMITS PER DWG 65-16346. ALODINED AND PRIMED AREAS.
- [SDR 96FDEA01132](https://openairdocs.org/sdr/96FDEA01132.md): Stringer · corroded · Jun 14, 1996 · N199FE · Boeing 727173C · Fuselage Main, Longeron/Stringer
  > NR 0032 AND 010. CORROSION (C53-113-10-1) ON STRINGER 26L, BS 680 TO BS 700. REMOVED CORRODED STR 26L, BS 668 - BS 740. INSTALLED REPAIR STR SECTION IAW FEDEX SRM 53-10-3.
- [SDR 96FDEA01126](https://openairdocs.org/sdr/96FDEA01126.md): Spar Chord · cracked · Jun 13, 1996 · N199FE · Boeing 727173C · Wing Spar
  > NR 0490 AND 009. LEFT WING AFT UPPER SPAR CHORD VERTICAL LEG HAS CRACK BETWEEN NR 2 AND NR 3 SPOILERS. REMOVED DAMAGE FROM LEFT WING UPPER REAR SPAR STA 531 - 539. FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 57-10-6, MM 27-61-0, MM 28-1-0.
- [SDR 96FDEA01109](https://openairdocs.org/sdr/96FDEA01109.md): Frame · cracked · Jun 12, 1996 · N199FE · Boeing 727173C · Fuselage Main, Frame
  > NR0535 AND 007, WHILE WORKING NR0032 FOUND FRAME TO BE CRACKED AT BS 680 LBL 30 STR 26L. *S/D* REPAIRED CRACKED FRAME AT BS 680 STR 26L PER SRM 51-40-3.
- [SDR 96FDEA01060](https://openairdocs.org/sdr/96FDEA01060.md): Shear Tie · crack · May 31, 1996 · N199FE · Boeing 727173C · Fuselage Structure (General)
  > SHEAR TIE CRACKED STA 328 WL 231 BETWEEN STR 21 TO 13R, AREA MARKED. REMOVED CRACKED SHEAR TIE, FABRICATED NEW SHEAR TIE, TREATED ALL BARE METAL AND INSTALLED AT BS 328 WL 231 BETWEEN STR 12 TO13R PER FEDEX SRM 53-10-4.
- [SDR 96FDEA01059](https://openairdocs.org/sdr/96FDEA01059.md): Skin · dented · May 31, 1996 · N199FE · Boeing 727173C · Fuselage Main, Plate/Skin
  > DENT IN SKIN BS 403 BETWEEN STR 21 AND 22R. DENT FOUND TO BE OUT OF LIMIT PER FEDEX SRM 53-30-1. CUT OUT DAMAGE, FABRICATED REPAIR PART, TREATED ALL BARE METAL AND INSTALLED ON SKIN AT BS 403 BETWEEN STR 21 AND 22R PER FEDEX SRM 53-30-3.
- [SDR 96FDEA00946](https://openairdocs.org/sdr/96FDEA00946.md): Bonding Jumper · corrosion · May 10, 1996 · N199FE · Boeing 727173C · Trailing Edge Flaps
  > NR0477 AND 003, NR 6 K-FLAP O/B BONDING JUMPER BETWEEN K-FLAP AND L/E STRUCTURE HAS CORROSION AROUND LOWER MOUNT POINT.
- [SDR 96FDEA00932](https://openairdocs.org/sdr/96FDEA00932.md): Bonding Jumper · corrosion · May 9, 1996 · N199FE · Boeing 727173C · Leading Edge Devices
  > NR0265 AND 002, NR 6 K-FLAP I/B BONDING JUMPER BETWEEN BULLNOSE AND K-FLAP HAS CORROSION AT BOTH MOUNT POINTS. *S/D* REMOVED AND REPLACED NR 6 K-FLAP ON FEDEX NR0477.
- [SDR 96FDEA00931](https://openairdocs.org/sdr/96FDEA00931.md): Bonding Jumper · corroded · May 9, 1996 · N199FE · Boeing 727173C · Leading Edge Devices
  > NR0264 AND 001, NR 4 K-FLAP I/B BONDING JUMPER BETWEEN K-FLAP AND BULLNOSE HAS CORROSION ON UPPER MOUNT BRACKET. *S/D* REPAIRED NR 4 K-FLAP I/B BONDING JUMPER UPPER ATTACH POINT IAW FEDEX SRM 57-50-3.
- [SDR 96FDEA00204](https://openairdocs.org/sdr/96FDEA00204.md): Shear Tie · corrosion · Feb 9, 1996 · N199FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 LBL 17 TO 22, FOUND WHILE WORKING NR 0053 WL 146.

## 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 = 'N199FE' AND deregistration_id = 'N199FE-2004-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N199FE-2004-08-16/reports

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