# Service difficulty reports: N102FE, cancelled Aug 26, 2004

A list on [N102FE, cancelled Aug 26, 2004](https://openairdocs.org/deregistered/N102FE-2004-08-26.md).

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

- [SDR 00FDEA00480](https://openairdocs.org/sdr/00FDEA00480.md): Jackscrew · damaged · Jul 20, 2000 · N102FE · Boeing 72722C · Trailing Edge Flap Control System
  > ON T/O AND DURING FLAP RETRACTION I/B FLAPS STUCK JUST PRIOR TO FLAPS 2 ON GAUGE CAUSING SPLIT TRAILING EDGE FLAP MALFUNCTION. RED TABS PROC COMPLIED WITH. FOUND RT I/B JACK SCREW END BROKEN AND ELEPHANT EAR JAMMED BETWEEN FLAP AND A/C. *S/D* REMOVED AND R
- [SDR 00FDEA00325](https://openairdocs.org/sdr/00FDEA00325.md): Actuator · inoperative · May 9, 2000 · N102FE · Boeing 72722C · Leading Edge Slat Actuator
  > AT CR ''A'' SYSTEM HYD QTY WENT TO ZERO, GEAR UP AND FLAPS UP. SHUT OFF ENGINE PUMPS (1 & 2) AND FLUID SHUT OFF (1 & 2) CRANKED GEAR DOWN. *S/D* REMOVED AND REPLACED NR 5 SLAT ACTUATOR AND NR 1 ENG A SYS HYD PUMP PER 727 MM 29-11-033-4, 29-11-033-5, 29-11-0
- [SDR 00FDEA00245](https://openairdocs.org/sdr/00FDEA00245.md): Smoke · detected · Apr 14, 2000 · N102FE · Boeing 72722C · Smoke Detection
  > CREW REPORTS SMOKE/FUMES IN COCKPIT, EMERGENCY DECLARED. *S/D* REMOVED AND REPLACED NR 1 & 2, 02 BOTTLES PER IAW MM 35-10.
- [SDR 98FDEA00223](https://openairdocs.org/sdr/98FDEA00223.md): Outflow Valve · failed · Mar 31, 1998 · N102FE · Boeing 72722C · Pressure Regulator/Outflow Valve
  > AIRCRAFT WILL NOT PRESSURIZE IN NORMAL OR AUTOMATIC. NO AUTHORITY WITH MANUAL WITH FULL INCREASE PRESSURE. CABIN VERTICAL SPEED INDICATOR FULL CLIMB THROUGHOUT. *S/D* REPLACED LEFT OUTFLOW VALVE PER MAINTENANCE MANUAL 21-30-51, PERFORMED SYSTEM ADJUSTMENT
- [SDR 98FDEA00033](https://openairdocs.org/sdr/98FDEA00033.md): Connector · dirty · Jan 14, 1998 · N102FE · Boeing 72722C · Landing Gear Position and Warning
  > THE RIGHT GEAR DOOR REMAINED OPEN AFTER GEAR HANDLE WAS PLACED UP. AFTER 2 MIN THE GEAR WAS RECYCLED PER RED TABS. THE RIGHT GEAR DOOR CONSISTENTLY IS SLOW TO CLOSE 2 MIN IN ON PAST 3 LANDINGS. OPERATED RIGHT GEAR DOOR PER MAINTENANCE MANUAL 32-62 DOOR TEST
- [SDR 97FDEA00100](https://openairdocs.org/sdr/97FDEA00100.md): Doubler · corroded · Feb 11, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0578 031, CORROSION (C53-221-01) ON COCKPIT FLOOR AND ON ATTACHED ANGLE AT BS 225, RBL 20 TO 26. *S/D* REMOVED CORROSION ON COCKPIT FLOOR AND ATTACHED ANGLE AT BS 225, RBL 20 TO 26 PER FED-EX SRM 51-10-6. FOUND TO BE OUT OF LIMITS IN VARIOUS AREAS PER FE
- [SDR 97FDEA00099](https://openairdocs.org/sdr/97FDEA00099.md): Frame · corroded · Feb 11, 1997 · N102FE · Boeing 72722C · Fuselage Main, Frame
  > NR 0633 030, CORROSION (53-221-01) AT FRAME STA 227 AFT O/B ANGLE, WL 235 RT. *S/D* REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED, FABRICATED AND INSTALLED FRAME AT STA 227 AT WL 235 RT SIDE. ALL WORK ACCOMPLISHED PER FED-EX
- [SDR 97FDEA00095](https://openairdocs.org/sdr/97FDEA00095.md): Ceiling Support · corroded · Feb 7, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0357 028. CORROSION (C53-111-01) ON CENTER CEILING SUPPORT FROM BS 660 TO BS 500, WL 200 BL ZERO. REMOVED CORROSION FROM CEILING SUPPORT STABILIZER BS 500 TO 660, BL ZERO, WL 199 AND FOUND OUT OF LIMITS IN NUMEROUS AREAS PER FED-EX SRM 53-10-1. REMOV
- [SDR 97FDEA00082](https://openairdocs.org/sdr/97FDEA00082.md): Floorbeam · corroded · Feb 1, 1997 · N102FE · Boeing 72722C · Fuselage Main, Floor Beam
  > NR 0283 027. CORROSION C53-224-01(1) ON FLOORBEAM UPPER FLANGE BOTTOM FWD SIDE AT BS 360, LBL 56, WL 207.8. REPAIRED FLOORBEAM AT BS 360, LBL 56, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED PER FED-EX SRM 53-10-8 FIG 8.
- [SDR 97FDEA00074](https://openairdocs.org/sdr/97FDEA00074.md): Shear Tie · cracked · Jan 27, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0707 021. WHILE WORKING NR 0083, FOUND CRACKED SHEAR TIE AT BS 278, STR 26 LT. CRACKED SHEAR TIE AT BS 278. STRINGER 26 LT FABRICATED NEW SHEAR TIE AND INSTALLED I.A.W. FED-EX SRM 53-10-4.
- [SDR 97FDEA00073](https://openairdocs.org/sdr/97FDEA00073.md): Clip · corroded · Jan 27, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0703 022. WHILE WORKING NR 00831 FOUND STRINGER CLIP AT BS 295 STR 26 TO BE CORRODED BEYOND LIMITS. REMOVED AND FABRICATED STRINGER CLIP I.A.W. FED-EX SRM 727 53-10-3. ALODINE AND PRIMED I.A.W. FED-EX 727 51-10-2. INSTALLED I.A.W. FED-EX SRM 727 51-1
- [SDR 97FDEA00089](https://openairdocs.org/sdr/97FDEA00089.md): Stringer · corroded · Jan 25, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0122 025 CORROSION (C53-224-01,3) ON STRINGER 4 RT AT BS 978 TO 1040 AND BS 1090 TO 1110. *S/D* REMOVED AND REPLACED STRINGER 4 RT FROM BS 950 TO 1120 IAW FED-EX SRM 53-10-3.
- [SDR 97FDEA00069](https://openairdocs.org/sdr/97FDEA00069.md): Stringer · corroded · Jan 23, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0705 019. WHILE WORKING NR 0083 FOUND STR 25 LT TO BE CORRODED BEYOND LIMITS BS 310. REMOVED CORRODED STRINGER FROM BS 295 TO BS 360 STR 25 LT AND INSTALLED NEW STRINGER FROM BS 295 TO 360, STR 25 LT I.A.W. FED-EX SRM 53-10-2 AND SRM 51-30-2, 51-10-1.
- [SDR 97FDEA00068](https://openairdocs.org/sdr/97FDEA00068.md): Skin · corroded · Jan 23, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/Skin
  > NR 0706 017. WHILE WORKING NR 00083, FOUND SKIN AT BS 225-360 STR 25 LT-28 LT TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED SKIN FROM BS 225-360, STR 25 LT AND INSTALLED NEW SKIN PANEL I.A.W. BOEING DRAWING NR-18420 AND FED-EX 727 SRM 53-10-1.
- [SDR 97FDEA00067](https://openairdocs.org/sdr/97FDEA00067.md): Angle · corroded · Jan 23, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0704 018 WHILE WORKING NR 0083 FOUND LOWER FLANGE OF LT LOWER NOSE ANGLE TO BE CORRODED AROUND NUTPLATE HOLES BS 330 TO 350. *S/D* LT LOWER NOSE ANGLE AND TEE ANGLE WERE FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED NOSE ANGLE AN
- [SDR 97FDEA00077](https://openairdocs.org/sdr/97FDEA00077.md): Stringer · cracked · Jan 22, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0701 023 NR 6 RT STRINGER CRACKED AT BS 400. *S/D* CUT OUT DAMAGED NR 6 STRINGER FROM BS 390 TO BS 410, FABRICATED AND INSTALLED REPAIR PARTS PER FED-EX SRM 53-10-3.
- [SDR 97FDEA00063](https://openairdocs.org/sdr/97FDEA00063.md): Frame · dented · Jan 22, 1997 · N102FE · Boeing 72722C · Fuselage Main, Frame
  > NR 0508 013 DAMAGED FRAME AT BS 990 BETWEEN STR 526-R AND 527-R. *S/D* REMOVED DAMAGED AREA OF 1 BY 1.75. FABRICATED REPAIR DOUBLER IAW 727 FED-EX SRM 51-40-3. INSTALLED REPAIR DOUBLER IAW FED-EX SRM 51-40-3 AND 51-30-2 BETWEEN STR 27 AND 26 RT BS 990.
- [SDR 97FDEA00062](https://openairdocs.org/sdr/97FDEA00062.md): Frame · dented · Jan 22, 1997 · N102FE · Boeing 72722C · Fuselage Main, Frame
  > NR 0509 014 DAMAGED FRAME AT BS 1010 BETWEEN STR 27 AND 26 RT. *S/D* REMOVED DAMAGED, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 51-40-3 AT BS 1010 BETWEEN STR 27 AND 26 RT.
- [SDR 97FDEA00060](https://openairdocs.org/sdr/97FDEA00060.md): Stringer · corroded · Jan 22, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0125 16 CORROSION (C53-224-01,3) ON STRINGER 4 LT BS 990 TO 1030 AND BS 1080 TO 1110. *S/D* FOUND CORROSION ON STRINGER 4 LT TO BE OUT OF LIMITS AT BS 1050 TO 1120. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS PER FED-EX SRM 53-10-3.
- [SDR 97FDEA00079](https://openairdocs.org/sdr/97FDEA00079.md): Stringer · cracked · Jan 21, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0700 024 NR 5 RT STRINGER CRACKED AT BS 400. *S/D* CUT OUT DAMAGED NR 5 STRINGER FROM BS 390 TO BS 410, FABRICATED AND INSTALLED REPAIR PARTS PER FED-EX SRM 53-10-3.
- [SDR 97FDEA00061](https://openairdocs.org/sdr/97FDEA00061.md): Skin · corroded · Jan 21, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/Skin
  > NR 0345 015. CORROSION (C53-224-01) ON INTERNAL SKIN AT BS 560-580, STR 1-9 RT, BS 540-560 BETWEEN STR 3 LT AND 4 RT, BS 500-520 BETWEEN STR 3 LT AND 2 LT BS, 460-480 BETWEEN STR 3-2 LT AND STR 1-2 RT ACCESS IS REQUIRED. REMOVED CORROSION ON INTERNAL SKIN
- [SDR 97FDEA00053](https://openairdocs.org/sdr/97FDEA00053.md): Skin · damage · Jan 20, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/Skin
  > NR 0237 007. SKIN CREASED AT ST 188, WL 181 RT, BS 180 TO 185, WL 179 AND BS 198, WL 182 RT. REMOVED DAMAGED SKIN AND FABRICATED REPAIR PARTS. INSTALLED FILLERS AND DOUBLER I.A.W. FED-EX SRM 727-53-30-3, SEALED FAYING SURFACES I.A.W. FED-EX SRM 727-51-20-4
- [SDR 97FDEA00056](https://openairdocs.org/sdr/97FDEA00056.md): Chord · corroded · Jan 18, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0687 010. WHILE WORKING CUSTOMER CARD NR 0083 FOUND CORROSION ON CHORD BS 219, LBL 26, WL 173. REMOVED OLD CHORD, FABRICATED NEW CHORD PARTS, ALODINED, PRIMED I.A.W. FED-EX SRM 51-40-4. REPAIRED WEB BY FABRICATING WEB REPAIR PLATE I.A.W. FED-EX SRM 51-
- [SDR 97FDEA00054](https://openairdocs.org/sdr/97FDEA00054.md): Floorbeam · corroded · Jan 17, 1997 · N102FE · Boeing 72722C · Fuselage Main, Floor Beam
  > NR 0516 009. CORROSION (53-111-01) UNDER NUTPLATE AT BS 1050, LBL 19, WL 200. ACCOMPLISHED REPAIR TO FLOORBEAM AT BS 1050, LBL 19 AND RBL 30, WL 200 PER FED-EX E.A. NR 7-5310-32136A, WITH APU AND PACKS ON, PERFORMED LEAK CHECK, NO LEAKS FOUND. FUNCTIONAL
- [SDR 97FDEA00044](https://openairdocs.org/sdr/97FDEA00044.md): Skin · corroded · Jan 12, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0615 006. CORROSION (C53-221-01) AT STA 245 UNDER CAPTAIN'S NR 3 WINDOW, WL 227. REMOVED CORROSION 3 INCH BY 4 INCH BY.049 INCH FROM ORIGINAL THICKNESS OF.065 INCH. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED DAMAGED AREA AND INSTALLE
- [SDR 97FDEA00041](https://openairdocs.org/sdr/97FDEA00041.md): Floorbeam · corrosion · Jan 12, 1997 · N102FE · Boeing 72722C · Fuselage Main, Floor Beam
  > NR 0515 005 CORROSION (C53-111-01) UNDER NUTPLATE AT BS 1148, RBL 1, WL 200. *S/D* CORROSION WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1148, WL 200, RBL 1 PER FED-EX SRM 53-10-1 AND SRM 53-10-8.
- [SDR 97FDEA00040](https://openairdocs.org/sdr/97FDEA00040.md): Floorbeam · corrosion · Jan 10, 1997 · N102FE · Boeing 727222 · Fuselage Main, Floor Beam
  > NR 0284 004 CORROSION (C53-224-01,1) ON FLOORBEAM AROUND NUTPLATE HOLES BS 380 LBL 45 TO 55, WL 207.5. *S/D* REPAIRED FLOORBEAM BS 380, LBL 31 TO LBL 70, WL 208 IAW FED-EX SRM 53-10-8 FIG 5. CORROSION FOUND TO BE OUT OF LIMITS.
- [SDR 97FDEA00098](https://openairdocs.org/sdr/97FDEA00098.md): Floorbeam · corroded · Jan 9, 1997 · N102FE · Boeing 72722C · Fuselage Main, Floor Beam
  > NR 0288 029, CORROSION (C53-224-01,1) ON FLOORBEAM BS 640, LBL 12, WL 208 AND BLI AROUND FLOORBOARD FASTENER HOLES. *S/D* REPAIRED BEAM AT BS 640, LBL 60 TO RBL 25. REPAIRED SEAT TRACK AT BS 630 TO BS 660, LBL 55. ACCOMPLISHED WEB REPAIR BS 600 TO BS 660,
- [SDR 97FDEA00031](https://openairdocs.org/sdr/97FDEA00031.md): Skin · corrosion · Jan 9, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/Skin
  > NR 083 003 CORROSION (C53-100-01) AT LAP LT STA 211 TO STA 259.5 STRINGER 25. *S/D* REMOVED CORROSION FROM SKIN AT LAP STA 211 TO STA 259.5, STR 19 TO 24 LT AND FOUND OUT OF LIMITS PER FED-EX SRM 53-30-1. REPAIRED SKIN PER FED-EX SRM 53-30-3 FIG 3A AND FED-
- [SDR 97FDEA00083](https://openairdocs.org/sdr/97FDEA00083.md): Angle · double holes · Jan 8, 1997 · N102FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0637 026. WHILE WORKING 7-5300-7-230YM1 PT 3, FOUND EXISTING DOUBLE HOLE IN L-ANGLE BS 925-950, LBL 63, WL 200. REMOVED L- ANGLE. FABRICATED NEW ANGLE, DRILLED, TREATED AND INSTALLED FASTENERS I.A.W. BAC DWG 65-18745, 65-18332 AND FED-EX SRM 51-10-1.
- [SDR 97FDEA00058](https://openairdocs.org/sdr/97FDEA00058.md): Frame · cracked · Jan 8, 1997 · N102FE · Boeing 72722C · Emergency Exits
  > NR 0609 012 FWD LT OVERWING EXIT LOWER WENCE FRAME, HAS A CRACK BETWEEN FASTENER HOLES AT O/B EDGE OF FRAME THAT ATTACHES TO OUTER SKIN. *S/D* REMOVED AND REPLACED FWD LT OVERWING EXIT, FWD LOWER CORNER FRAME IAW FED-EX SRM 51-30-2.
- [SDR 97FDEA00057](https://openairdocs.org/sdr/97FDEA00057.md): Bulkhead Angle · cracked · Jan 8, 1997 · N102FE · Boeing 72722C · Fuselage Main, Bulkhead
  > NR 0618 011 CORROSION BS 178 BULKHEAD L-ANGLE LBL 28, WL 208 TO WL 224. *S/D* REMOVED CORROSION AND FOUND CHORD L-ANGLE TO BE CRACKED. REMOVED CHORD AND REPLACED PER FED-EX SRM 51-10-1, 51-30-2.
- [SDR 97FDEA00030](https://openairdocs.org/sdr/97FDEA00030.md): Stringer · corrosion · Jan 8, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0595 002 CORROSION (C53-224-01) ON STRINGER 4 RT BS 460 TO 360. *S/D* REMOVED DAMAGED STR 4 RT, BS 410 TO 450. FABRICATED NEW PARTS AND INSTALLED PER FED-EX 727 SRM 53-10-3.
- [SDR 97FDEA00070](https://openairdocs.org/sdr/97FDEA00070.md): Stringer · corroded · Jan 7, 1997 · N102FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > NR 0353 020. CORROSION (C53-224-01) ON STRINGER 2 RT BS 560-BS 520. REMOVED CORRODED STRINGER 2 RT FROM BS 510-570 AND FABRICATED AND INSTALLED REPAIR PARTS ON AIRCRAFT PER FED-EX SRM 53-10-3.
- [SDR 97FDEA00055](https://openairdocs.org/sdr/97FDEA00055.md): Skin · corroded · Jan 6, 1997 · N102FE · Boeing 72722C · Fuselage Main, Plate/Skin
  > NR 0356 008. CORROSION (C53-224-05) ON UPPER SURFACE OF CENTER WING TANK AT BS 757, RBL 65, WL 204. REMOVED CORROSION AND REPAIRED I.A.W. FED-EX E.A. NR 7-5710-32133.
- [SDR 97FDEA00027](https://openairdocs.org/sdr/97FDEA00027.md): Frame · corroded · Jan 6, 1997 · N102FE · Boeing 72722C · Fuselage Main, Frame
  > NR 0367 001 CORROSION (C53-111-01, 2) ON TOP OF FRAME AT BS 680, WL 156, LBL 20.5. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED MATERIAL AND REPAIRED CORRODED FRAME AT BS 680, WL 156, LBL 20.5 IAW FED-EX SRM 51-40-3.
- [SDR 95FDEA01135](https://openairdocs.org/sdr/95FDEA01135.md): Adi · failed · Aug 17, 1995 · N102FE · Boeing 72722C · Attitude Gyro and Indicating System
  > CAPTAIN'S ADI FAILED DURING CLIMB OUT IN NORMAL POSITION, AND ALSO FAILED IN AUXILIARY POSITION. REPLACED CAPTAIN'S ADI. OPS CK NORMAL ON GROUND.

## 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 = 'N102FE' AND deregistration_id = 'N102FE-2004-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N102FE-2004-08-26/reports

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