# Service difficulty reports: N192FE, cancelled May 2, 2007

A list on [N192FE, cancelled May 2, 2007](https://openairdocs.org/deregistered/N192FE-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 2 · 53 reports

- [SDR 06FDEA1958](https://openairdocs.org/sdr/06FDEA1958.md): Skin · corroded · May 17, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > LOWER SKIN OF LEFT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO I/B END, FWD SRAP TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1941](https://openairdocs.org/sdr/06FDEA1941.md): Beam · chafed · May 17, 2006 · N192FE · Boeing 72722 · Elevator Structure
  > WHILE GETTING AND OK TO CLOSE, FOUND RT ELEVATOR RUB BLOCK SPACER LOOSE AND CHAFING INTO LOWER TRAILING EDGE BEAM AT ELEV STA 118.13. REPAIRED RT HORIZ STAB LOWER TRAILING EDGE BEAM AT ELEV STA 118.13 IAW FED EX EA 7- 5510-100932.
- [SDR 06FDEA1928](https://openairdocs.org/sdr/06FDEA1928.md): Door Frame · corroded · May 15, 2006 · N192FE · Boeing 72722 · Fuselage Main, Structure
  > LEFT AFT EMERGENCY EXIT SEAL FRAME CORRODED. FOUND CORROSION ON SEAL FRAME TO BE OUT OF LIMITS. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH PER MM 52-21-000-5.
- [SDR 06FDEA1911](https://openairdocs.org/sdr/06FDEA1911.md): Attach Fitting · corroded · May 12, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 2 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REMOVED, REPAIRED AND REINSTALLED NR 2 FLAP TRACK FWD ATTACH FITTING IAW OHM 20-50-01 ANS FED EX EA 7-5710-96623.
- [SDR 06FDEA1800](https://openairdocs.org/sdr/06FDEA1800.md): Skin · damaged · May 11, 2006 · N192FE · Boeing 727100 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB HAS A BLEND OUT THAT EXCEEDS SRM LIMITS AT STAB STA 77.1,.500 FWD OF THE EDGE OF THE T/E SKIN. REPAIRED LT HORIZONTAL STAB LWR SKIN PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1799](https://openairdocs.org/sdr/06FDEA1799.md): Skin · corroded · May 11, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > FOUND LOWER SKIN OF RIGHT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO IB END, FWD SPAR TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1777](https://openairdocs.org/sdr/06FDEA1777.md): Skin · dented · May 10, 2006 · N192FE · Boeing 727100 · Cargo/Baggage Doors
  > LWR FWD CARGO DOOR FWD EDGE OF EXTERIOR SKIN HAS SEVERAL DENTS. *S/D* REMOVED AND REPLACED LWR FWD CARGO DOOR IAW FED EX MM 52-31-000-4.
- [SDR 06FDEA1738](https://openairdocs.org/sdr/06FDEA1738.md): Attach Fitting · unknown · May 8, 2006 · N192FE · Boeing 727100 · Wing, Attach Fittings
  > N01182 COMPLY WITH EO 7-5710-7-2314D PT5- WINGS MLG TRUNION ATTATCH FITTING MODIFICATION SB 727-57A0132R3 AD 2004-18-08, LT SIDE. COMPLIED WITH FED EX EO 7-5710-7-2314D PT 5 AND FED-EX EA 7-5710-96632.
- [SDR 06FDEA1724](https://openairdocs.org/sdr/06FDEA1724.md): Fitting · cracked · May 5, 2006 · N192FE · Boeing 72722 · Fuselage Main, Attach Fittings
  > WHILE INSPECTING BS 870 RT TERMINAL FITTING PER FED EX EO 7-5310-7-3663 03 PART 4 FOUND CRACK INDICATION IN ROW 3 HOLE NR 5. REPAIRED DAMAGED HOLE BS 870 TERMINAL FITTING ROW 3, HOLE NR 5 PER FED EX EA 7-5310-99513.
- [SDR 06FDEA1702](https://openairdocs.org/sdr/06FDEA1702.md): Frame · gouged · May 4, 2006 · N192FE · Boeing 727100 · Fuselage Main, Frame
  > LWR FWD CARGO DOOR CUTOUT AFT SIDE FRAME IS GOUGED FWD OF LATCH FITTING STR 23 RT. REPAIRED LOWER FWD CARGO DOOR CUTOUT AFT SIDE FRAME IAW FED EX EA 7-5310-99516.
- [SDR 06FDEA1703](https://openairdocs.org/sdr/06FDEA1703.md): Skin · corroded · May 4, 2006 · N192FE · Boeing 727100 · Trailing Edge Flaps
  > LT WING, I/B MID FLAP UPPER SKIN IS CORRODED, 4 INCHES FROM T/E AND 12 INCHES AND 58 INCHES FROM I/B END. *S/D* REMOVED & REPLACED FLAP PER FED EX MM 27-51-013.
- [SDR 06FDEA1697](https://openairdocs.org/sdr/06FDEA1697.md): Flap Track · damaged · May 3, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 6 FLAP TRACK AFT ATTACH FITTING DAMAGED OB BARREL NUT HOLE. REMOVED AND REPLACED NR 6 FLAP TRACK AFT O/B ATTACH FITTING PER SRM 51-30-02 AND SRM 51-20-01.
- [SDR 06FDEA1655](https://openairdocs.org/sdr/06FDEA1655.md): Floorbeam · corroded · May 1, 2006 · N192FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND 1110 FLOORBEAM CORRODED ON LOWER FLANGE LBL 30 TO RBL 30. REMOVED AND REINSTALLED AFT CARGO BAY CEILING PANELS BS 1110 TO BS 1170 AND REMOVED AND REINSTALLED FLOORBOARDS BS 1030 TO BS 1100 RBL 0 TO RBL 45 FOR ACCESS IAW SRM 51-30-2. FOUND CORROSION
- [SDR 06FDEA1664](https://openairdocs.org/sdr/06FDEA1664.md): Support Fitting · corroded · May 1, 2006 · N192FE · Boeing 727100 · Nacelle/Pylon, Main Frame
  > NR 1 ENG PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON HAS CORROSION ON FWD AND AFT SIDES IN SEVERAL AREAS. COMPLIED WITH FED EX EA 7-5410-99512 ON NR 1 ENGINE PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON ON FWD AND AFT SIDES.
- [SDR 06FDEA1663](https://openairdocs.org/sdr/06FDEA1663.md): Support Fitting · corroded · May 1, 2006 · N192FE · Boeing 727100 · Nacelle/Pylon, Main Frame
  > NR 1 ENG PYLON HAS CORROSION ON FWD ENG SUPPORT FITTING WEB FWD LWR I/B JUST ABOVE LWR HORIZONTAL FLANGE COMMON TO EO 7-5410-7-3304 P9 PAGE 12 FIG 2. *S/D* COMPLIED WITH FED EX EA 7-5410-99512.
- [SDR 06FDEA1662](https://openairdocs.org/sdr/06FDEA1662.md): Flange · corroded · May 1, 2006 · N192FE · Boeing 727100 · Engine Mount Section
  > NR 1 ENG PYLON ON FWD ENG SUPPORT HORIZONTAL FLANGE HAS CORROSION ON UPPER FWD EDGE. *S/D* COMPLIED WITH FED EX EA 7-5410-99512.
- [SDR 06FDEA1612](https://openairdocs.org/sdr/06FDEA1612.md): Stringer Clip · corroded · Apr 26, 2006 · N192FE · Boeing 727100 · Fuselage Main, Attach Fittings
  > STA 380 STR 19L CORROSION ON STR CLIP. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 380, STR 19L, PER SRM 51-30-2.
- [SDR 06FDEA1578](https://openairdocs.org/sdr/06FDEA1578.md): Shear Tie · cracked · Apr 24, 2006 · N192FE · Boeing 72722 · Fuselage Internal Mounting Structure
  > FOUND CRACK IN OEM SHEAR TIE AT BS 520 ABOVE STR 22L. REPAIRED OEM SHEAR TIE AT BS 520 ABOVE STR 22L IAW SRM 53-10-04.
- [SDR 06FDEA1576](https://openairdocs.org/sdr/06FDEA1576.md): Shear Tie · corroded · Apr 24, 2006 · N192FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > STA 1030 STR 29R, CORROSION ON FRAME OUTBOARD FLANGE. *S/D* REMOVED AND REPLACED SHEAR TIE ON BS 1030, STR 29R FRAME OUTBOARD FLANGE IAW SRM 53-10-4.
- [SDR 06FDEA1577](https://openairdocs.org/sdr/06FDEA1577.md): Structure · cracked · Apr 24, 2006 · N192FE · Boeing 727100 · Fuselage Main, Structure
  > BS 961, RBL 10, STR 29R AT BS 961, RBL 10, STR 29R, STRUCTURE IS CRACKED. REMOVED DAMAGE AND REPAIRED CHORD PER SRM 51-40-04.
- [SDR 06FDEA1566](https://openairdocs.org/sdr/06FDEA1566.md): Frame · corroded · Apr 21, 2006 · N192FE · Boeing 727100 · Fuselage Main, Frame
  > STA 970 BETWEEN STR 29L AND STR 30, CORROSION ON FRAME OUTBOARD FLANGE. *S/D* REPAIRED PER SRM 53-10-4.
- [SDR 06FDEA1486](https://openairdocs.org/sdr/06FDEA1486.md): Skin · delaminated · Apr 17, 2006 · N192FE · Boeing 727100 · Trailing Edge Flaps
  > RIGHT WING I/B FORE FLAP DELAMINATED MID SPAN ON UPPER SURFACE. *S/D* REPAIRED DELAM ON UPPER SURFACE ON RIGHT WING I/B FORE FLAP PER SRM 51-40-20.
- [SDR 06FDEA1455](https://openairdocs.org/sdr/06FDEA1455.md): Web · gouged · Apr 14, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND FUSELAGE BS 480 TO 640, STR 3L, CARGO DOOR SURROUND WEB GOUGED IN NUMEROUS AREAS. ALL WORK ACCOMPLISHED IAW FEDEX EA 7-5330-99510.
- [SDR 06FDEA1422](https://openairdocs.org/sdr/06FDEA1422.md): Web · corroded · Apr 12, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR WEB, BS 1130 TO 1176 RBL 49 TO 63, WL 208. REPAIRED FLOOR WEB AT BS 1130 TO 1176 RBL 49 TO 63, WL 208 IAW SRM 51-40-02.
- [SDR 06FDEA1360](https://openairdocs.org/sdr/06FDEA1360.md): Bulkhead · cracked · Apr 10, 2006 · N192FE · Boeing 727100 · Fuselage Main, Bulkhead
  > CRACK IN BULKHEAD AT BS 870, LBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870, LBL 12, WL 138 IAW SRM 53-10-9 FIG 4.
- [SDR 06FDEA1359](https://openairdocs.org/sdr/06FDEA1359.md): Bulkhead · cracked · Apr 10, 2006 · N192FE · Boeing 727100 · Fuselage Main, Bulkhead
  > CRACK IN BULKHEAD AT BS 870, RBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870 RBL 12 WL 138 IAW SRM 53-10-9 FIG 4.
- [SDR 06FDEA1358](https://openairdocs.org/sdr/06FDEA1358.md): Support Angle · cracked · Apr 10, 2006 · N192FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > FOUND CRACK ON LOWER SUPPORT ANGLE AT BS 870 LBL 12 WL 138. REPAIRED CRACKED ANGLE AT BS 870 RBL 12 WL 138 IAW SRM 54-10-9.
- [SDR 06FDEA1363](https://openairdocs.org/sdr/06FDEA1363.md): Keelbeam · corroded · Apr 10, 2006 · N192FE · Boeing 72722 · Fuselage Main, Floor Beam
  > STA 1030 - 1050 STR 29R HAS CORROSION ON STR FLANGE.
- [SDR 06FDEA1362](https://openairdocs.org/sdr/06FDEA1362.md): Keelbeam · corroded · Apr 10, 2006 · N192FE · Boeing 72722 · Fuselage Main, Keel
  > FOUND STA 1034 STR 29L, CORROSION ON STR FLANGE AT RIVET TAIL.
- [SDR 06FDEA1361](https://openairdocs.org/sdr/06FDEA1361.md): Web · tool damage · Apr 10, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND DRILL START BEHIND VERTICAL STIFFENER ON FWD SIDE OF 870 WEB.
- [SDR 06FDEA1337](https://openairdocs.org/sdr/06FDEA1337.md): Web · corroded · Apr 7, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR WEB, BS 1155, RBL 41, WL 208. REPAIRED PER SRM 51-40-02.
- [SDR 06FDEA1335](https://openairdocs.org/sdr/06FDEA1335.md): Gusset · damaged · Apr 7, 2006 · N192FE · Boeing 727100 · Fuselage Main, Structure
  > UPON REMOVAL OF SHEAR WEB AT BS 1176, FOUND GUSSET TO BE DAMAGED AROUND LUG AT BS 1176, WL 208, LBL 18. *S/D* REMOVED AND REPLACED GUSSET BS 1176, LBL 18, WL 208 IAW SRM 51-40-2.
- [SDR 06FDEA1336](https://openairdocs.org/sdr/06FDEA1336.md): Skin · dented · Apr 7, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENT BS 693, 5" BELOW STR 26R. REPAIRED PER SRM 53-30-3.
- [SDR 06FDEA1334](https://openairdocs.org/sdr/06FDEA1334.md): Skin · corroded · Apr 7, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 120,.5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REPAIR FROM FEDEX NR N00382 (TAIL 5008). REPAIRED RT HORIZ STAB AT RT STAB STA 120,.5" AFT OF THE L
- [SDR 06FDEA1333](https://openairdocs.org/sdr/06FDEA1333.md): Skin · corroded · Apr 7, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > FOUND RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 116.5, 9.5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REPAIR FROM FEDEX NR N00382 (TAIL 5008). REPAIRED PER SRM 55-10-3.
- [SDR 06FDEA1332](https://openairdocs.org/sdr/06FDEA1332.md): Skin · chafed · Apr 7, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF FAIRING 3509 FOR ACCESS FOUND EXTERNAL FUSELAGE SKIN CHAFED AT FAIRING CONTACT LINE, BS 1110-1130 BETWEEN STR 25 AND 26 LEFT. REPAIRED PER SRM 53-30-3.
- [SDR 06FDEA1321](https://openairdocs.org/sdr/06FDEA1321.md): Stringer · corroded · Apr 6, 2006 · N192FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > FOUND STA 970 - 1030, CORROSION IN STR 30 AT RIVET TAILS. REPAIRED STR 30 PER SRM 53-10-3.
- [SDR 06FDEA1313](https://openairdocs.org/sdr/06FDEA1313.md): Flap Track · corroded · Apr 5, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 6 FLAP TRACK IS CORRODED AT SAFETY BOLT HOLE. REPLACED NR 6 FLAP TRACK IAW TASK CARD 27X5708-03.
- [SDR 06FDEA1307](https://openairdocs.org/sdr/06FDEA1307.md): Angle · corroded · Apr 4, 2006 · N192FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > STA 348 LBL 17 WL 149, CORROSION ON LOWER NOSE ANGLE (AFT OF NLG). REMOVED AND REPLACED CHORD AT STA 348 LBL 17 WL 149 IAW SRM 51-30-2.
- [SDR 06FDEA1279](https://openairdocs.org/sdr/06FDEA1279.md): Frame · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Fuselage Main, Frame
  > FOUND STA 1070 BETWEEN STR 28L AND 29L, CORROSION ON FRAME OUTBOARD FLANGE. REPAIRED FRAME BS 1070 STR 28L TO 29L IAW SRM 53-10-4.
- [SDR 06FDEA1300](https://openairdocs.org/sdr/06FDEA1300.md): Flap Track · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 8 FLAP TRACK FWD LUG IS CORRODED. REPLACED NR 8 FLAP TRACK IAW TASK CARD 27X5710-03.
- [SDR 06FDEA1299](https://openairdocs.org/sdr/06FDEA1299.md): Skin · damaged · Apr 3, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND STA 342, 4" BELOW STR 21L SKIN HAS SHARP PROTRUSION, FROM APPARENT INTERNAL IMPACT. REPAIRED DAMAGE AT STA 342 4" BELOW STR 21L IAW SRM 53-30-3 FIG 13A.
- [SDR 06FDEA1281](https://openairdocs.org/sdr/06FDEA1281.md): Flap Track · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 7 FLAP TRACK CORRODED AT FWD END. REPLACED NR 7 FLAP TRACK IAW TASK CARD 27X5709-03.
- [SDR 06FDEA1280](https://openairdocs.org/sdr/06FDEA1280.md): Web · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR WEB, BS 1146 TO 1173, LBL 7 TO 14, WL 208. REPLACED FLOOR WEB, BS 1146-1173 WL 208 PER SRM 51-30-2, 51-10-2, 51-20-4.
- [SDR 06FDEA1246](https://openairdocs.org/sdr/06FDEA1246.md): Skin · dented · Mar 27, 2006 · N192FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > N00969 DENT IN SKIN, BS 748, JUST BELOW STR2R. REPAIRED DENT PER FED EX E.A. 7-5330-96624
- [SDR 06FDEA1247](https://openairdocs.org/sdr/06FDEA1247.md): Skin · dented · Mar 27, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND DENT IN SKIN, BS 1084, 1" ABOVE STR 2L TO 4" ABOVE STR 4L. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-99514 FOUND TO BE A MAJOR REPAIR
- [SDR 05FDEA02746](https://openairdocs.org/sdr/05FDEA02746.md): Skin · damaged · Sep 4, 2005 · N192FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166-1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED EX EA 7-5330-91350.
- [SDR 05FDEA02706](https://openairdocs.org/sdr/05FDEA02706.md): Skin · cracked · Aug 29, 2005 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166 - 1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED EX EA 7-5330-91350.
- [SDR 05FDEA02705](https://openairdocs.org/sdr/05FDEA02705.md): Skin · dented · Aug 29, 2005 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > WHILE WORKING ON AIRCRAFT, RAN INTO AIRCRAFT N192FE. DENTED AT BS 1203L TO 1223L IN BETWEEN STRINGERS 19 & 20, GOUGED AT BS 1203L TO 1223L IN BETWEEN STRINGERS 20 & 21. REPAIRED SKIN PER SRM 53-30-3, MAJOR REPAIR.
- [SDR 05FDEA02425](https://openairdocs.org/sdr/05FDEA02425.md): Pitot Line · obstructed · Aug 11, 2005 · N192FE · Boeing 72722 · Pitot/Static System
  > AFTER TAKE F/O NOTED AIRSPEED INDICATOR STOPPED ACCELERATING BEYOND 140 KTS AS CAPTAIN LEVEL AT 3000, F/O ALTIMETER READ 2000 F/O AIRSPEED INOP FLAG CAME INTO VIEW. NO C/B'S OUT. F/O SELECTED ALTERNATE STATIC SOURCE THEN F/O'S A.S AND ALTIMETER THEN MATCHED

Next page: https://openairdocs.org/deregistered/N192FE-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 = 'N192FE' AND deregistration_id = 'N192FE-2007-05-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N192FE-2007-05-02/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.