# Service difficulty reports: N188FE, cancelled Apr 25, 2007

A list on [N188FE, cancelled Apr 25, 2007](https://openairdocs.org/deregistered/N188FE-2007-04-25.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 · 119 reports

- [SDR 05FDEA04265](https://openairdocs.org/sdr/05FDEA04265.md): Accessory Unit · failed · Dec 12, 2005 · N188FE · Boeing 72722 · Landing Gear Position and Warning
  > DURING TEST FLIGHT, HAD NO LEFT MAIN GEAR INDICATION. PERFORMED GOOD RING OUT PER FED EX WDM 32-64-02, 32-64-01. REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED GOOD FUNCTIONAL TEST PER FED EX MM 20-10-017-2, 32-09-111-5.
- [SDR 05FDEA04242](https://openairdocs.org/sdr/05FDEA04242.md): Rod · dirty · Dec 12, 2005 · N188FE · Boeing 727100 · Landing Gear Position and Warning
  > DURING TEST FLIGHT WITH GEAR HANDLE UP NOSE GEAR RED LIGHT AND RED DOORS LIGHT STAYED ON. *S/D* CLEANED DIRT FROM AND LUBRICATED NLG DOOR SWITCH ACTUATOR RODS. JACKED NOSE AND SWUNG GEAR. NLG FUNCTIONALLY TESTED GOOD. SERVICED NLG STRUT. WORK DONE PER MM
- [SDR 05FDEA04188](https://openairdocs.org/sdr/05FDEA04188.md): Skin · damaged · Dec 8, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > REWORK REQUIRED, FROM NR01182. ACCOMPLISH REPAIR PER FEDEX ENGINEERING, BS 480, STR 26L-27L. *S/D* COMPLIED WITH FED EX EA 7-5330-95353, FOUND TO BE A MAJOR REPAIR.
- [SDR 05FDEA03997](https://openairdocs.org/sdr/05FDEA03997.md): Repair · improper · Nov 28, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > REPAIR AT BS 694, STR 19R REQUIRES ENGINEERING DISPOSITION IAW EO 7-5100-7- 5000 PT1. ACCOMPLISHED REPAIR AT BS 694 STR 19R PER FED EX E.A. 7-5330-91416.
- [SDR 05FDEA03859](https://openairdocs.org/sdr/05FDEA03859.md): Rib · mislocated · Nov 17, 2005 · N188FE · Boeing 72722 · Elevator Structure
  > WHILE WORKING CARD N01365, FOUND RT NR 5 ELEVATOR HINGE RIB MISLOCATED. REMOVED AND REPLACED RT NR 5 ELEVATOR HINGE RIB PER EA 7-5510-91413.
- [SDR 05FDEA03858](https://openairdocs.org/sdr/05FDEA03858.md): Fitting · corroded · Nov 17, 2005 · N188FE · Boeing 727100 · Main Landing Gear
  > LEFT MLG FWD TRUNNION SUPPORT FITTING O/B FLANGE, O/B SURFACE HAS SURFACE CORROSION BETWEEN -THROUGH PIN- AND LWR PORK CHOP FITTING BOLT HOLE LOCATIONS. REPAIRED L/H MLG FWD TRUNNION SUPPORT FITTING PER FED EX EA 7-5710-91408.
- [SDR 05FDEA03835](https://openairdocs.org/sdr/05FDEA03835.md): Rib · damaged · Nov 16, 2005 · N188FE · Boeing 72722 · Horizontal Stabilizer, Spar/Rib
  > DURING INSPECTION OF THE LT HORIZ STAB ELEVATOR RIB AT ELEV STA 136.5, FOUND TO HAVE EXISTING REPAIRS ON THE LOWER IB AND OB FLANGES OF THE RIB AT THE TRAILING EDGE BEAM. RIB REQUIRES REPLACEMENT PER FEDEX EO 7-5510-7-5001 PT 1. REPAIRED PER S.B. 727-55A00
- [SDR 05FDEA03801](https://openairdocs.org/sdr/05FDEA03801.md): Repair · unknown · Nov 14, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > REPAIR AT BS 480 STR 26L TO 27L REQUIRES ENGINEERING DISPOSITION PER EO 7- 5100-7-5000 P3. COMPLIED WITH FED-EX EA 7-5330-95353. FOUND TO BE MAJOR REPAIR
- [SDR 05FDEA03615](https://openairdocs.org/sdr/05FDEA03615.md): Stringer · unknown · Nov 3, 2005 · N188FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > STR 25R REQUIRES ENGINEERING DISPOSITION PER EO 7-5100-7-5000 PT1. COMPLIED WITH E.A. 7-5330-91409
- [SDR 05FDEA03614](https://openairdocs.org/sdr/05FDEA03614.md): Frame · damaged · Nov 3, 2005 · N188FE · Boeing 72722 · Fuselage Main, Frame
  > FUSELAGE, MAIN FRAME FORWARD CARGO DOOR FORWARD FRAME REPLACEMENT AD'S 90-06-09 AND 98-11-03 R1 (LOG BOOK ENTRY REQUIRED). REPAIRED PER E.A. 7-5310-93709
- [SDR 05FDEA03560](https://openairdocs.org/sdr/05FDEA03560.md): Floorbeam · corroded · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND CORROSION (C53-224-01) ON MAIN CARGO DECK FLOORBEAM UPPER AND LOWER FLANGE AT BS 1130 BETWEEN RBL 25 AND RBL 45, WL 208. REPAIRED MAIN DECK FLOORBEAM UPPER FLANGE AT BS 1130, RBL 45, WL 208 REF SRM 53-10- 8 FIG 10.
- [SDR 05FDEA03562](https://openairdocs.org/sdr/05FDEA03562.md): Skin · cracked · Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > BS 1352 RT SKIN CRACK AT RAIN GUTTER LOCATION. REPAIRED PER SRM 54-30-2
- [SDR 05FDEA03553](https://openairdocs.org/sdr/05FDEA03553.md): Failsafe · cracked · Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, Frame
  > BS 1010 FRAME IS CRACKED AT STRINGER 25 LEFT. REPAIRED PER SRM 51-40-3
- [SDR 05FDEA03552](https://openairdocs.org/sdr/05FDEA03552.md): Failsafe · cracked · Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, Frame
  > BS 990 FRAME IS CRACKED AT STRINGER 25 RIGHT. REPAIRED PER SRM 51-40-3
- [SDR 05FDEA03551](https://openairdocs.org/sdr/05FDEA03551.md): Failsafe · cracked · Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, Frame
  > N01348 BS 990 FRAME IS CRACKED TWO PLACES AT STRINGER 25 LT. REPAIRED PER SRM 51-40-3
- [SDR 05FDEA03549](https://openairdocs.org/sdr/05FDEA03549.md): Support · corroded · Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY CEILING SUPPORT BS 1107 RBL 6 WL 200. REPAIRED PER SRM 53-10-1
- [SDR 05FDEA03548](https://openairdocs.org/sdr/05FDEA03548.md): Shear Tie · corroded · Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE BS 990 LBL 3 WL 148. REPAIRED PER SRM 53-10-2
- [SDR 05FDEA03559](https://openairdocs.org/sdr/05FDEA03559.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10L. REPAIRED PER E.O. 7-5330-7-2319 PT 5
- [SDR 05FDEA03558](https://openairdocs.org/sdr/05FDEA03558.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10R. REPAIRED PER E.O. 7-5330-7-2319 PT 5
- [SDR 05FDEA03557](https://openairdocs.org/sdr/05FDEA03557.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 261 STR 14R. REPAIRED PER E.O. 7-5330-7-2319 PT 5
- [SDR 05FDEA03556](https://openairdocs.org/sdr/05FDEA03556.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 19. REPAIRED PER E.O. 7-5330-7-2319 PT 5
- [SDR 05FDEA03555](https://openairdocs.org/sdr/05FDEA03555.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 1081 STR 10L. REPAIRED PER E.O. 7-5330-7-2313F PT 5
- [SDR 05FDEA03554](https://openairdocs.org/sdr/05FDEA03554.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Cargo/Baggage Doors
  > FOUND FORWARD CARGO DOOR HAS MULTIPLE SCRATCHES ON EXTERIOR SKIN IN THE UNPAINTED AREA. REPAIRED PER E.A. 7-5230-91411.
- [SDR 05FDEA03550](https://openairdocs.org/sdr/05FDEA03550.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT BS 1081 STR 10R. REPAIRED PER E.O. 7-5330-7-2313 PT 5
- [SDR 05FDEA03504](https://openairdocs.org/sdr/05FDEA03504.md): Frame · damaged · Oct 26, 2005 · N188FE · Boeing 727100 · Fuselage Main, Frame
  > UPPER LOBE INTERIOR FRAME HAS MACH DAMAGE AND OPEN HOLES BS 890 STR 9L. [OPEN]
- [SDR 05FDEA03491](https://openairdocs.org/sdr/05FDEA03491.md): Skin · cracked · Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE OUTER SKIN STA 591 STR 15R FWD UPPER CORNER OF WING L/E ILLUMINATION LIGHT CUT OUT. REPAIRED PER FED EX EA 7-5330-95384.
- [SDR 05FDEA03490](https://openairdocs.org/sdr/05FDEA03490.md): Floorbeam · corroded · Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor Beam
  > BS 480 FLOORBEAM UPPER CHORD CORRODED AT RBL 48, WL 208. [OPEN]
- [SDR 05FDEA03489](https://openairdocs.org/sdr/05FDEA03489.md): Intercostal · cracked · Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > N01148 CRACK BS 660 STR 2L UPPER INTERCOSTAL EXTENSION. [OPEN]
- [SDR 05FDEA03487](https://openairdocs.org/sdr/05FDEA03487.md): Frame · damaged · Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Frame
  > N00737 FRAME BS 990 BTWN STR 22 LT- 24 LT DAMAGED. [OPEN]
- [SDR 05FDEA03481](https://openairdocs.org/sdr/05FDEA03481.md): Frame · dented · Oct 24, 2005 · N188FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO BAY FRAME BS 1030 BETWEEN STR 26 LT AND 27 LT DENTED. FABRICATED DOUBLER CAP AT BS 1030 BTWN STR 26 AND 27 L/H USING 7075T6.071 M590750 PER SRM 51-40-3. INSTALLED DOUBLER CAP AT BS 1030 BETWEEN STR 26 AND STR 27 LT PER SRM 51-30-2.
- [SDR 05FDEA03480](https://openairdocs.org/sdr/05FDEA03480.md): Shear Tie · corroded · Oct 24, 2005 · N188FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMP SHEAR TIE IS CORRODED BS 1130 RBL 8 WL 152. REPAIRED PER SRM 53-10-4.
- [SDR 05FDEA03448](https://openairdocs.org/sdr/05FDEA03448.md): Floorbeam · cracked · Oct 18, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor Beam
  > N00474 E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 CRACK EXTENDING UP FROM STOP DRILL. STOP DRILLED CRACK AND REPAIRED WEB AT CRACK IN E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 IAW SRM 51-10-1 AND SRM 51-40-2
- [SDR 05FDEA03442](https://openairdocs.org/sdr/05FDEA03442.md): Shear Web · cracked · Oct 17, 2005 · N188FE · Boeing 727100 · Fuselage Main, Structure
  > WHILE WORKING CARD N00368 FOUND SHEAR WEB 8-5-825, RBL 65-70, WL 208 TO BE CRACKED. SHEAR WEB BS 805-825 RBL 65-70 W/L 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2. SRM 51-30-5, SRM 51-10-2.
- [SDR 05FDEA03441](https://openairdocs.org/sdr/05FDEA03441.md): Skin · cracked · Oct 17, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND EXTERNAL SKIN CRACKED AT F/O'S NR 5 WINDOW CUT OUT AT UPPER AFT FASTENER HOLE. INSTALLED REPAIR DOUBLER F/O'S NR 5 WINDOW CUT OUT UPPER AFT CORNER IAW SRM 53-30-3.
- [SDR 05FDEA03433](https://openairdocs.org/sdr/05FDEA03433.md): Skin · gouged · Oct 14, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND GOUGE IN SKIN AT STR 20L BS 368. REPAIRED GOUGE IN SKIN AT STR 20L BS 368 PER SRM 53-30-3 FIG 3.
- [SDR 05FDEA03432](https://openairdocs.org/sdr/05FDEA03432.md): Skin · dented · Oct 14, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND BS 465 STR 19L HAS A DENT. REPAIRED STR 19L AT BS 465 PER SRM 51-30-2 AND 53-10-3.
- [SDR 05FDEA03425](https://openairdocs.org/sdr/05FDEA03425.md): Shear Tie · damaged · Oct 13, 2005 · N188FE · Boeing 72722 · Fuselage Internal Mounting Structure
  > FOUND BS 620 STR 25 LT DAMAGE AROUND FASTENER ON SHEAR TIE THROUGH SKIN. REMOVED AND REPLACED SHEAR TIE AT BS 620 STR 25 LH IAW SRM 51-10-2, 51-20, AND SRM 51-30-2.
- [SDR 05FDEA03424](https://openairdocs.org/sdr/05FDEA03424.md): Stringer · cracked · Oct 13, 2005 · N188FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > FOUND UPPER LOBE INTERIOR STRINGER IS CRACKED BS 480 STR 16R. REMOVED AND REPLACED WITH NEW STR. SECTION IAW SRM 53-30-2 AND SRM 53-10-4.
- [SDR 05FDEA03423](https://openairdocs.org/sdr/05FDEA03423.md): Stringer Clip · damaged · Oct 13, 2005 · N188FE · Boeing 72722 · Fuselage Main, Attach Fittings
  > FOUND MAIN CARGO DECK STRINGER CLIP IS DAMAGED AT BS 440, STR 8L. REMOVED AND REPLACED MAIN CARGO DECK STRINGER CLIP BS 440 STR 8L IAW SRM 51-30-2.
- [SDR 05FDEA03422](https://openairdocs.org/sdr/05FDEA03422.md): Stringer Clip · gouged · Oct 13, 2005 · N188FE · Boeing 72722 · Fuselage Main, Attach Fittings
  > FOUND MAIN CARGO COMPARTMENT STRINGER CLIP GOUGED BS 380 STR 6R. REMOVED AND REPLACED MAIN CARGO COMPARTMENT STRINGER CLIP BS 380, STR 6R IAW SRM 51-30-2.
- [SDR 05FDEA03410](https://openairdocs.org/sdr/05FDEA03410.md): Floorbeam · corroded · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION BS 344 FLOORBEAM LBL 55 TO RBL 10. REPAIRED BS 344 FLOORBEAM LBL 55 TO RBL 10 PER FED-EX DWG SR 27-53-007.
- [SDR 05FDEA03409](https://openairdocs.org/sdr/05FDEA03409.md): Web · cracked · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > WHILE WORKING N01046 FOUND WEB AT BS 344 LBL 32 CRACKED. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-02 ON WEB AT BS 344 LBL 32.
- [SDR 05FDEA03408](https://openairdocs.org/sdr/05FDEA03408.md): Floor Panel · corroded · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Floor Panel
  > CORROSION ON MAIN CARGO DECK FLOOR PANEL WEB AT BS 1150, RBL 60, WL 208. CUT OUT DAMAGE FLOOR WEB AT BS 1150, RBL 60, WL 208 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2.
- [SDR 05FDEA03407](https://openairdocs.org/sdr/05FDEA03407.md): Web · gouged · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > HAYES MOD WEB GOUGED AT 9 PLACES BETWEEN STR 5L AND STR 13L BS 620. REPAIRED GOUGES STR 5L AND 13L, BS 620 HAYES MOD WEB PER SRM 53-10-2, 51-40-2, 51-30- 2.
- [SDR 05FDEA03406](https://openairdocs.org/sdr/05FDEA03406.md): Web · gouged · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > HAYES MOD WEB GOUGED AT BS 640L AT STR 12L AND 14L.
- [SDR 05FDEA03405](https://openairdocs.org/sdr/05FDEA03405.md): Stringer · damaged · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > UPPER LOBE INTERIOR SIDE OF STRINGER IS DAMAGED BS 782 STR 4L. REPAIRED STRINGER AT B.S. 782 STR 4L PER SRM 53-10-1.
- [SDR 05FDEA03404](https://openairdocs.org/sdr/05FDEA03404.md): Floorbeam · corroded · Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION BS 328 FLOORBEAM AT FASTENER HOLES. CORROSION ON FLOORBEAM AT B.S. 328 LBL 22 WAS OUT OF LIMITS REPAIRED FLOORBEAM PER FED EX EA 7-5310-91401.
- [SDR 05FDEA03393](https://openairdocs.org/sdr/05FDEA03393.md): Shear Tie · corroded · Oct 11, 2005 · N188FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMP SHEAR TIE IS CORRODED BS 1110 RBL 8 WL 150.
- [SDR 05FDEA03392](https://openairdocs.org/sdr/05FDEA03392.md): Floorbeam · corroded · Oct 11, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION BS 360 FLOORBEAM BL 0. REJECTED BECAUSE CORROSION AND BARE METAL STILL PRESENT ON BOTTOM SIDE OF UPPER CHORD AND BL 0. REPAIRED PER SRM 53-10-8.
- [SDR 05FDEA03391](https://openairdocs.org/sdr/05FDEA03391.md): Floorbeam · corroded · Oct 11, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION AFT CARGO BAY FLOORBEAM LWR CHORD BS 1110 RBL 4 - 24 WL 200. CUT OUT DAMAGE ON LWR FLANGE OF BS 1110 FLOORBEAM RBL 2-RBL 26. FABRICATED AND INSTALLED REPAIR IAW FEDEX SR DRAWING SR 27-53-034E.

Next page: https://openairdocs.org/deregistered/N188FE-2007-04-25/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 = 'N188FE' AND deregistration_id = 'N188FE-2007-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N188FE-2007-04-25/reports

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