# Service difficulty reports: N191FE, cancelled May 2, 2007

A list on [N191FE, cancelled May 2, 2007](https://openairdocs.org/deregistered/N191FE-2007-05-02.md).

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

Page 1 of 3 · 147 reports

- [SDR 07FDEA00427](https://openairdocs.org/sdr/07FDEA00427.md): Computer · malfunctioned · Feb 8, 2007 · N191FE · Boeing 72722 · Stall Warning System
  > CAPT STICK SHAKER ACTIVATED ON ROTATION. SHAKER SPEED WAS ABNORMALLY SLOW, ABOUT 1/3 NORMAL RATE DURING TEST. SHAKER CONTINUED FOR APPROX 3 MINUTES AND SLOWED GRADUALLY UNTIL IT STOPPED. AIRCRAFT FLEW NORMALLY. REMOVED AND REPLACED NR 1 STALL WARNING COMPU
- [SDR 06FDEA0889](https://openairdocs.org/sdr/06FDEA0889.md): Skin · cracked · Mar 2, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145. *S/D* REMOVED REPAIR BS 352, LBL 18, WL 145, REPAIRED IAW FED EX EA 7-5330-96595.
- [SDR 06FDEA0844](https://openairdocs.org/sdr/06FDEA0844.md): Skin · damaged · Feb 26, 2006 · N191FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DENT WITH ASSOCIATED GOUGE IN FUSELAGE SKIN, BS 590, BETWEEN STR 17 AND 18 RT. FOUND TO BE OUT OF SERVICE LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A.
- [SDR 06FDEA0814](https://openairdocs.org/sdr/06FDEA0814.md): Skin · debonded · Feb 23, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > N01287 REWORK OF CARD N01229 REQUIRED. WHILE INSPECTING LT LOWER NOSE CHORD INSTALLATION, FOUND SKIN DISBONDED AND CORRODED AT BS 297, LBL 20, WL 148. REWORK REQUIRED BECAUSE REPAIR WAS INSTALLED IN A RESTRICTED AREA IAW SRM 53-30-3 FIG. 12. ** SD **
- [SDR 06FDEA0806](https://openairdocs.org/sdr/06FDEA0806.md): Shear Tie · damaged · Feb 22, 2006 · N191FE · Boeing 72722 · Fuselage Internal Mounting Structure
  > WHILE REMOVING SKIN FOR ACCESS ON STR 27L REPAIR; FOUND SHEAR TIE AT BS 1143 STR 27L DAMAGED. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 15.
- [SDR 06FDEA0578](https://openairdocs.org/sdr/06FDEA0578.md): Stringer · corroded · Feb 7, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > WHILE WORKING N01286 FOUND STRINGER 27 LEFT CORRODED AT BS 1176. REMOVED AND REPLACED STR 27L, BS 1090 - 1183 IAW SRM 53-10-3, 51-10-2, AND 51-30-2.
- [SDR 06FDEA0537](https://openairdocs.org/sdr/06FDEA0537.md): Spar · tool damage · Feb 3, 2006 · N191FE · Boeing 72722 · Wing Spar
  > RT WING FRONT SPAR LOWER CHORD PLATE HAS A MISSED DRILLED HOLE LOCATED DIRECTLY BELOW THE NR 4 K-FLAP ACTUATOR. REPAIRED MISSDRILLED HOLE IAW FED EX EA 7-5710-96565.
- [SDR 06FDEA0467](https://openairdocs.org/sdr/06FDEA0467.md): Angle · unknown · Feb 1, 2006 · N191FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH EA 7-5710-96564, RIGHT MAIN LANDING GEAR TRUNNION SUPPORT FITTING, -TEE ANGLE- HOLE LOCATION -E- REPAIR- AD 2004-18-08. COMPLIED WITH FED-EX EA 7-5710-96564, REFERENCE CUSTOMER CARD 7-5710-7-2314 PT 4.
- [SDR 06FDEA0431](https://openairdocs.org/sdr/06FDEA0431.md): Web · damaged · Jan 30, 2006 · N191FE · Boeing 727100 · Vertical Stabilizer
  > WHILE WORKING FED EX CARD N00897 FOUND AN EXTRA HOLE ON WEB UNDER UPPER PANEL SUPPORT CHORD ON VERTICAL STAB AT FIN STA 247 UPPER RIGHT SIDE. *S/D* REPAIRED PANEL SUPPORT CHORD ON VERTICAL STAB IAW FED-EX EA 7-5530-96566.
- [SDR 06FDEA0430](https://openairdocs.org/sdr/06FDEA0430.md): Skin · unknown · Jan 30, 2006 · N191FE · Boeing 727100 · Aircraft Structures
  > DURING ACCESS FOR STR 30 REPAIR, (CUSTOMER CARD N00999), UPON REMOVAL OF EXISTING REPAIR DOUBLER BS 1165 - 1183 RBL 12 - LBL 10 FOUND ORIGINAL SKIN HAS CUTOUT BS 1175 - 1183 RBL 1 - 6.5 AND BS 1183 LWR CHORD CUTOUT IN A 1 X 2 INCH AREA. ALL WORK WAS ACCOMPLISH
- [SDR 06FDEA0404](https://openairdocs.org/sdr/06FDEA0404.md): Spar · corroded · Jan 27, 2006 · N191FE · Boeing 727100 · Wing Spar
  > RT WING FRONT SPAR HAS AREAS OF CORROSION AT LES 340-345. REPAIRED PER FED EX EA 7-5710-96562.
- [SDR 06FDEA0405](https://openairdocs.org/sdr/06FDEA0405.md): Trunnion · unknown · Jan 27, 2006 · N191FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > WHILE WORKING E.O. 705710-7-2314 P4, FOUND BOTH "C" HOLES IN TRUNION ATTACH FITTING TO BE SPOTFACED ON INNER SURFACE AROUND HOLES. REPAIRED RT MLG FWD TRUNNION FITTING SPOT FACED AREAS AT "C" HOLE LOCATIONS IAW FED-EX EA 7-5710-96561. THIS IS A MAJOR REP
- [SDR 06FDEA0375](https://openairdocs.org/sdr/06FDEA0375.md): Flap · corroded · Jan 25, 2006 · N191FE · Boeing 727100 · Leading Edge Devices
  > NR 5 K-FLAP HAS CORROSION AT OB BULLNOSE TO K-FLAP BONDING WIRE BOTH ATTACH POINTS. REPAIRED NR 5 K FLAP BULLNOSE PER SR DRAWING SR 27-57-010 REV C.
- [SDR 06FDEA0374](https://openairdocs.org/sdr/06FDEA0374.md): Stringer · corroded · Jan 25, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, CORROSION ON STR. 30 BS 1166 TO BS 1183 BL 0. REPAIRED STR 30 BS 1140 - 1183 IAW SRM 53-10-3, 51-10-2 AND 51-30-2.
- [SDR 06FDEA0298](https://openairdocs.org/sdr/06FDEA0298.md): Structure · corroded · Jan 20, 2006 · N191FE · Boeing 727100 · Fuselage Main, Structure
  > WHILE WORKING N01170 FOUND CORROSION ON EXTERIOR FUSELAGE STRUCTURE AT BS 352, LBL 17, WL 145. REMOVED AND REPLACED STRUCTURE IAW SRM 53-10-1, 51-30-2.
- [SDR 06FDEA0304](https://openairdocs.org/sdr/06FDEA0304.md): Flap Track · corroded · Jan 20, 2006 · N191FE · Boeing 727100 · Trailing Edge Flaps
  > CORROSION ON NR 2 FLAP TRACK, AFT O/B MOUNTING HOLE. NEW NR 2 FLAP TRACK WAS INSTALLED ON FED-EX W/C 27X5706-03.
- [SDR 06FDEA0286](https://openairdocs.org/sdr/06FDEA0286.md): Door Frame · corroded · Jan 19, 2006 · N191FE · Boeing 727100 · Emergency Exits
  > CORROSION ON RIGHT FWD EMERGENCY EXIT HATCH EXTERIOR LWR EDGE FRAME UNDER PRESS SEAL. *S/D* RIGHT FWD EMERGENCY EXIT DOOR WAS OVERHAULED IAW WORK ORDER MR1382409.
- [SDR 06FDEA0214](https://openairdocs.org/sdr/06FDEA0214.md): Stringer · cracked · Jan 16, 2006 · N191FE · Boeing 727100 · Wing, Longeron/Stringer
  > LT WING, STA 629.00 THIRD STRINGER FROM REAR SPAR IS CRACKED.
- [SDR 06FDEA0181](https://openairdocs.org/sdr/06FDEA0181.md): Floorbeam · corroded · Jan 13, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION STA 312 LBL 30 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. *S/D* REPAIRED FLOORBEAM AT STA 312, LBL 30, WL 208 PER SRM 53-10-8, 53-10-1.
- [SDR 06FDEA0180](https://openairdocs.org/sdr/06FDEA0180.md): Floorbeam · corroded · Jan 13, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION STA 328 LBL 30 AND LBL 40 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. *S/D* REPAIRED FLOORBEAM AT BS 328, LBL 30 AND 40, WL 208 PER SRM 53-10-8, 53-10-1, 51-30-02.
- [SDR 06FDEA0157](https://openairdocs.org/sdr/06FDEA0157.md): Skin · cracked · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145. *S/D* REPAIRED SKIN IAW SRM 53-30-3.
- [SDR 06FDEA0155](https://openairdocs.org/sdr/06FDEA0155.md): Skin · dented · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > DENT IN EXTERNAL FUSELAGE SKIN AT BS 1163, STR 9L. *S/D* DENT IN FUSELAGE SKIN AT BS 1163, STR 9L REPAIRED IAW SRM 53-30-3.
- [SDR 06FDEA0158](https://openairdocs.org/sdr/06FDEA0158.md): Skin · cracked · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145.
- [SDR 06FDEA0156](https://openairdocs.org/sdr/06FDEA0156.md): Skin · cracked · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN HAS A CRACK AT FASTENER HOLE AT BS 352, RBL 18, WL 145. REPAIRED CRACK PER ER 06-1285 AND FED EX EA 7-5330-96592.
- [SDR 06FDEA0149](https://openairdocs.org/sdr/06FDEA0149.md): Shear Tie · corroded · Jan 11, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1110. *S/D* REMOVED FASTENERS COMMON TO SHEAR TIE, REMOVED CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4.
- [SDR 06FDEA0148](https://openairdocs.org/sdr/06FDEA0148.md): Skin · corroded · Jan 11, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > WHILE INSPECTING LT LOWER NOSE CHORD INSTALLATION FOUND SKIN DISBONDED AND CORRODED AT BS 297, LBL 20, WL 148.
- [SDR 06FDEA0135](https://openairdocs.org/sdr/06FDEA0135.md): Failsafe · cracked · Jan 10, 2006 · N191FE · Boeing 727100 · Fuselage Main, Structure
  > FAIL SAFE CHORD CRACKED BS 990 STR 25L. *S/D* CUT OUT AND REMOVED DAMAGED FAIL SAFE CHORD, FABRICATED AND INSTALLED REPAIR AND REPAIR SECTION PER SRM 51-40-3 FIG 1, IAW SRM 51-30-2.
- [SDR 06FDEA0134](https://openairdocs.org/sdr/06FDEA0134.md): Failsafe · cracked · Jan 10, 2006 · N191FE · Boeing 727100 · Fuselage Main, Structure
  > FAIL SAFE CHORD CRACKED BS 1030 STR 25L. *S/D* REMOVED FAIL SAFE CHORD, FABRICATED AND INSTALLED REPAIR AND REPAIRED SECTION PER SRM 51-40-3, 51-30-2.
- [SDR 06FDEA0131](https://openairdocs.org/sdr/06FDEA0131.md): Stringer · damaged · Jan 9, 2006 · N191FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT HOLE IN STR 23 LT B/S 965. REPAIRED AFT CARGO COMPARTMENT STR 23L AT BS 965, HOLE IN TOP OF STR IAW SRM 53-10-3.
- [SDR 06FDEA0104](https://openairdocs.org/sdr/06FDEA0104.md): Shear Tie · unknown · Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.
- [SDR 06FDEA0103](https://openairdocs.org/sdr/06FDEA0103.md): Shear Tie · corroded · Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR. 28 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.
- [SDR 06FDEA0102](https://openairdocs.org/sdr/06FDEA0102.md): Frame · corroded · Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > WHILE WORKING ON ACCESSING FOR N00743, FOUND CORROSION ON LT MIDDLE NOSE CHORD AT BS 297-BS 352, WL 169, LBL 16. ** SD ** COMING
- [SDR 06FDEA0060](https://openairdocs.org/sdr/06FDEA0060.md): Floorbeam · corroded · Jan 6, 2006 · N191FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOORBEAM UPPER FLANGE AROUND NUTPLATES AT BS 1130, LBL 10 TO RBL 29, WL 208. REPAIRED FLOORBEAM UPPER FLANGE BS1130, RBL 10, WL 208 IAW SRM 53-10-8.
- [SDR 06FDEA00019](https://openairdocs.org/sdr/06FDEA00019.md): Stringer · dented · Jan 4, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > DENTED STRINGER AT STA 493, STR 8RT. *S/D* REPAIRED STRINGER PER SRM 53-10-3.
- [SDR 06FDEA0018](https://openairdocs.org/sdr/06FDEA0018.md): Frame · tool damage · Jan 4, 2006 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, DRILL STARTS IN FRAME AT STR 23 RT AND 27 LT BS 1148 ON INBOARD FLANGE. *S/D* ALL MAINTENANCE REQUIREMENTS FOR THIS CARD ACCOMPLISHED ON CARD N00986.
- [SDR 06FDEA0015](https://openairdocs.org/sdr/06FDEA0015.md): Stringer · cracked · Jan 3, 2006 · N191FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > FOUND STR 26R CRACKED AT FASTENER HOLE O/B FLANGE BS 430. REPAIRED CRACKED FASTENER IAW SRM 53-10-03.
- [SDR 06FDEA0013](https://openairdocs.org/sdr/06FDEA0013.md): Skin · chafed · Jan 3, 2006 · N191FE · Boeing 72722 · Nacelle/Pylon, Plate/Skin
  > FOUND SECTION SKIN IS CHAFED ABOVE RT LWR RAIN GUTTER, BS 1351. REPAIRED SKIN CHAFE OVER RT LWR RAIN GUTTER, BS 1351 PER SRM 54-30-3.
- [SDR 06FDEA0012](https://openairdocs.org/sdr/06FDEA0012.md): Floorbeam · corroded · Jan 3, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor Beam
  > FOUND CORROSION, STA 344 LBL 50 TO RBL 15 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. REMOVED DAMAGED SECTION OF UPPER CHORD, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8.
- [SDR 05FDEA04412](https://openairdocs.org/sdr/05FDEA04412.md): Strap · corroded · Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > N00310 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130 RBL 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130, RBL 63, WL 208, PER SRM 51-30-2.
- [SDR 05FDEA04410](https://openairdocs.org/sdr/05FDEA04410.md): Strap · corroded · Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > N00312 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130 LBL. 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130, LBL 63, WL 208, IAW SRM 51-30-5, 51-30-2.
- [SDR 05FDEA04414](https://openairdocs.org/sdr/05FDEA04414.md): Skin · lightning strike · Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > N00280 LIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1167, STR 13R. DETERMINED LIGHTNING STRIKE DAMAGE IN SKIN AT BS 1167, STR 13R TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A.
- [SDR 05FDEA04413](https://openairdocs.org/sdr/05FDEA04413.md): Crease Beam · corroded · Dec 27, 2005 · N191FE · Boeing 727227 · Fuselage Main, Structure
  > FOUND CORROSION ON CREASE BEAM ANGLE, BS 1120 TO BS 1130, LBL 65, WL 208.
- [SDR 05FDEA04407](https://openairdocs.org/sdr/05FDEA04407.md): Frame · dented · Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 25 LT AND 27 LT BS 1050 ON IB FLANGE. REPAIRED DENTED FRAME BETWEEN STR 25LT AND 27LT, BS 1050 ON I/B FLANGE IAW SRM 51- 40-3.
- [SDR 05FDEA04406](https://openairdocs.org/sdr/05FDEA04406.md): Frame · dented · Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 24 LT AND 27 LT BS 1030 ON IB FLANGE. REPAIRED IAW SRM 51-40-3.
- [SDR 05FDEA04405](https://openairdocs.org/sdr/05FDEA04405.md): Frame · dented · Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 24 LT AND 27 LT BS 1010 ON IB FLANGE. REPAIRED PER 51-40-03 & 53-10-1.
- [SDR 05FDEA04404](https://openairdocs.org/sdr/05FDEA04404.md): Frame · dented · Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > N00987 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 26 LT AND 27 LT BS 1148 ON IB FLANGE ** SD ** COMING.
- [SDR 05FDEA04403](https://openairdocs.org/sdr/05FDEA04403.md): Frame · dented · Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 26 RT AND 23 RT BS, 1148 IN IB FLANGE. AFT CARGO COMPARTMENT FRAME AT BS 1148 BETWEEN STR 23R, AND 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-40-3.
- [SDR 05FDEA04402](https://openairdocs.org/sdr/05FDEA04402.md): Frame · dented · Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 25 LT AND 27 LT BS 990, ON IB FLANGE. REPAIRED FRAME PER SRM 51-40-3.
- [SDR 05FDEA04395](https://openairdocs.org/sdr/05FDEA04395.md): Structure · corroded · Dec 21, 2005 · N191FE · Boeing 72722 · Fuselage Main, Structure
  > BS 297 CORROSION ON LT LOWER NOSE CHORD.
- [SDR 05FDEA02932](https://openairdocs.org/sdr/05FDEA02932.md): Indicator · inoperative · Sep 15, 2005 · N191FE · Boeing 72722 · Leading Edge Slat Position Indicating System
  > NR 2 KRUGER FLAP LED FAILED TO RETRACT ON SCHEDULE. KRUGER FLAP INDICATION INOP, FO'S AND SO'S PANEL REMOVED AND REPLACED NR 2 POS INDICATION SWITCH PER MM 27-82-001-4 SYS, OPS CHECK NORMAL.

Next page: https://openairdocs.org/deregistered/N191FE-2007-05-02/reports.md?page=2

## 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 = 'N191FE' AND deregistration_id = 'N191FE-2007-05-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N191FE-2007-05-02/reports

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