# Service difficulty reports: N135FE, cancelled Aug 26, 2004

A list on [N135FE, cancelled Aug 26, 2004](https://openairdocs.org/deregistered/N135FE-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.

Page 1 of 2 · 53 reports

- [SDR 01FDEA00845](https://openairdocs.org/sdr/01FDEA00845.md): Slat · failed · Sep 18, 2001 · N135FE · Boeing 72725C · Leading Edge Slat Control System
  > UPON FLAP RETRACTION NR 6 SLAT FAILED TO RETRACT.
- [SDR 01FDEA00023](https://openairdocs.org/sdr/01FDEA00023.md): Switch · dirty · Jan 17, 2001 · N135FE · Boeing 72725C · Landing Gear Position and Warning
  > AFT T/O WITH GEAR RETRACT AND DOOR LIGHT OUT, HANDLE WAS PLACED IN OFF POSTION, RMG DOOR ILLUM. RAN RED TABS. PLACED HANDLE IN THE UP POSITION AND LIGHT WENT OUT. LT HANDLE IN UP POSITION. NO YAW OR NOISE ASSOCIATED WITH DOOR LIGHT ON. *S/D* CLEANED SWIT
- [SDR 00FDEA00808](https://openairdocs.org/sdr/00FDEA00808.md): Panel · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage Main, Structure
  > N 642-2 DURING ROUTINE INSP, THE AFT BAG BIN RIGHT TRANSISTION PANEL FOUND CORRODED AT RBL 23 FROM BS 1010-1030. R&R & FAB PER IAW BAC 7S7 SRM 51-40-2, 51-30-2.
- [SDR 00FDEA00805](https://openairdocs.org/sdr/00FDEA00805.md): Shear Tie · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage Main, Structure
  > DURING ROUTINE INSP, THE LOWER FUSELAGE SHEAR TIE FROM BS 196 - 203 AT RBL 6 FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 737 SRM 51-20-1, 51-30-2.
- [SDR 00FDEA00804](https://openairdocs.org/sdr/00FDEA00804.md): Spar · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Wing Spar
  > DURING ROUTINE INSP, CORROSION DAMAGE FOUND AT SEVERAL FASTENERS IN THE WING CENTER SECTION REAR SPAR UPPER CHORD. REMOVED AND REPLACED PER P/N 65-18538-5 IAW FEDEX EA 7-5710-53851.
- [SDR 00FDEA00803](https://openairdocs.org/sdr/00FDEA00803.md): Floorbeam · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > DURING ROUTINE INSP, THE BS 344 FLOORBEAM FOUND CORRODED BETWEEN NR 3 & 5 SEAT TRACKS. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-8.
- [SDR 00FDEA00802](https://openairdocs.org/sdr/00FDEA00802.md): Support Bracket · cracked · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, THE SUPPORT BRACKET ATTACHMENT FOR NOSE LANDING GEAR LOCK ACTUATOR WAS FOUND CRACKED AT BS 351.2. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2.
- [SDR 00FDEA00801](https://openairdocs.org/sdr/00FDEA00801.md): Support Bracket · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, THE SUPPORT BRACKET AT BS 1110, STR 19L FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 00FDEA00800](https://openairdocs.org/sdr/00FDEA00800.md): Intercostal · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > DURING ROUTINE INSP, THE LOWER FUSELAGE INTERCOSTAL AT RBL 23 FROM BS 1010 - 1030 FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-4, 51-30-2.
- [SDR 00FDEA00799](https://openairdocs.org/sdr/00FDEA00799.md): Seat Track · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE INSP, THE NR 1 SEAT TRACK FOUND CORRODED AT BS 783. REMOVED, REPLACED AND FAB PER IAW BAC 7S7 SRM 53-10-5, 51-30-2.
- [SDR 00FDEA00798](https://openairdocs.org/sdr/00FDEA00798.md): Seat Track · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE INSP, THE NR 6 SEAT TRACK FROM BS 737 - 740 CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.
- [SDR 00FDEA00797](https://openairdocs.org/sdr/00FDEA00797.md): Attach Angle · cracked · Nov 28, 2000 · N135FE · Boeing 72725C · Spoilers
  > DURING ROUTINE INPS, THE NR 12 SPOILER O/B ATTACH ANGLE FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2 & BAC SB 57-84.
- [SDR 00FDEA00796](https://openairdocs.org/sdr/00FDEA00796.md): Web · corroded · Nov 28, 2000 · N135FE · Boeing 72725C · Service Doors
  > DURING ROUTINE INSP, SERVICE DOOR FOUND CORRODED INSIDE THE SECOND LIGHTENING HOLE FROM FWD, APPROX WL 232.5. REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, 51-30-2, 52-12-00. OPS CK GOOD.
- [SDR 00FDEA00795](https://openairdocs.org/sdr/00FDEA00795.md): Skin · cracked · Nov 28, 2000 · N135FE · Boeing 72725C · Landing Gear Doors
  > DURING ROUTINE INSP, RT MAIN LANDING GEAR WING DOOR OUTER SKIN FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 52-80-2.
- [SDR 00FDEA00449](https://openairdocs.org/sdr/00FDEA00449.md): Switch · dirty · Jul 14, 2000 · N135FE · Boeing 72725C · Landing Gear Position and Warning
  > AFTER T/O, RAISING GEAR HANDLE LMG DOOR AND RED DOORS LIGHT REMAINS ON. FOUND MG DOOR SWITCH SOAKED WITH OIL. CLEANED CANNON PLUG AND RECONNECTED, CYCLED LEFT GEAR DOOR 4 TIMES, CHECKS OK.
- [SDR 02FDEA00320](https://openairdocs.org/sdr/02FDEA00320.md): Light · inoperative · May 8, 2000 · N135FE · Boeing 727200 · Landing Gear Position and Warning
  > DURING APPROACH TO CLE, L GEAR DOWN INDICATOR LIGHT (GREEN) DID NOT ILLUMINATE; NO OTHER ABNORMAL INDICATIONS. UNABLE TO REMOVE BULBS TO REPLACE. RECEIVED VISUAL CONFORMATION FROM TOWER THAT GEAR WAS DOWN; LANDED NORMALLY. RELAMPED ANNUNCIATOR. LIGHTS TES
- [SDR 98FDEA00770](https://openairdocs.org/sdr/98FDEA00770.md): Connector · contaminated · Dec 30, 1998 · N135FE · Boeing 72725C · Landing Gear Position and Warning
  > RIGHT MAIN GEAR DOOR LIGHT CAME ON AT 12,000 FT DURING DESCENT AT 340 KIAS. CYCLED GEAR AND ALL LIGHTS WENT OUT IND NORMAL. *S/D* REMOVED WATER FROM RIGHT GEAR DOOR LOCK CONDUIT. REMOVED AND REPLACED D752 CANNON PLUG, OPER CK GOOD AS PER MM 32-62-0.
- [SDR 98FDEA00302](https://openairdocs.org/sdr/98FDEA00302.md): Anti-Ice Duct · broken · Apr 20, 1998 · N135FE · Boeing 72725C · Engine Anti-Icing System
  > NR 2 ENGINE LEFT HAND ENGINE INLET ANTI-ICE DUCT BROKEN IN HALF. LOCATED JUST AFT OF ANTI-ICE VALVE. REMOVED AND REPLACED ANTI-ICE DUCT IAW FED-EX M/M 75-10-00.
- [SDR 98FDEA00278](https://openairdocs.org/sdr/98FDEA00278.md): Anti-Ice Duct · damaged · Apr 20, 1998 · N135FE · Boeing 72725C · Engine Anti-Icing System
  > NR 2 ENG LEFT HAND ENGINE INLET A/I DUCT DAMAGED, LOCATED JUST FWD OF THE A/I VALVE. *S/D* REMOVED AND REPLACED ANTI-ICE DUCT PER FED-EX M/M 75-10-14.
- [SDR 95FDEA01551](https://openairdocs.org/sdr/95FDEA01551.md): Rib · cracked · Oct 17, 1995 · N135FE · Boeing 72725C · Wing, Rib/Bulkhead
  > FWD UPPER HOLE AT 12 O'CLOCK ON THE RT RIB CHORD AT STA 760 IS CRACKED. REPAIRED PER EA 7-5710-25838 DATED 10-11-95.
- [SDR 95FDEA01550](https://openairdocs.org/sdr/95FDEA01550.md): Angle · cracked · Oct 17, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > FWD 2 HOLES IN LT CHORD ANGLE AT STA 760 SHOW CRACKS. REPAIR COMPLETED PER EA 7-5710-25838.
- [SDR 95FDEA01548](https://openairdocs.org/sdr/95FDEA01548.md): Fitting · cracked · Oct 15, 1995 · N135FE · Boeing 72725C · Fuselage, Wing Attach Fittings
  > LT WING FRONT SPAR FWD TERMINAL PIN JOINT HOLE CRACKED AFT END. LEVELED AND SHORED A/C IAW SRM 51-50-1, CUT LOWER CHORD ANGLE AND WEB IAW BOEING DRWG NR 65C29064, REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANG
- [SDR 95FDEA01488](https://openairdocs.org/sdr/95FDEA01488.md): Fitting Pin · corroded · Oct 4, 1995 · N135FE · Boeing 72725C · Wing, Fuselage Attach Fittings
  > RIGHT WING REAR SPAR BODY FITTING FWD AND REAR BUSHINGS WORN, BODY FITTING PIN FLANGE CORRODED. INSTALLED NEW RT WING REAR SPAR BODY FITTING PIN PER SRM 51-10-1 PG 4, REPLACED FWD AND REAR BUSHINGS PER 51-10-1 PG 4, ESO 11782 AND FEDEX EA NR 7-5310-25827.
- [SDR 95FDEA01487](https://openairdocs.org/sdr/95FDEA01487.md): Floor Beam · corroded · Oct 3, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION IN AFT CARGO COMP FS 1110 FLOOR BEAM LOWER FLANGE BL 16L TO 30L. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED FILLER AND DOUBLER PER ESO 11782, INSTALLED FILLER AND DOUBLER PER ESO 11782 AND SRM 51-10-6, 51-40-2. EA NR 7-5310-25810.
- [SDR 95FDEA01486](https://openairdocs.org/sdr/95FDEA01486.md): Floor Beam · corroded · Oct 3, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION IN LOWER FLANGE OF FLOOR BEAM BS 1110, BL 0 - 48 RT, IN AFT CARGO COMP. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED ANGLES AND STRAP PER ESO 11782, INSTALLED SAME PER ESO 11782, EA NR 7-5310-25188.
- [SDR 95FDEA01485](https://openairdocs.org/sdr/95FDEA01485.md): Skin · cracked · Oct 3, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > DOUBLER CRACKED AT RIVET STA 1160 O/B OF STR 26R. REMOVED DAMAGED SKIN AT SKIN LAP STA 1149 - 1163, STR 26R PER SRM 53-30-3 FIG 5. INSTALLED REPAIR DOUBLER FROM STA 1140 - 1167 STR 26R PER SRM 53-30-3, PAGES 20-25.
- [SDR 95FDEA01463](https://openairdocs.org/sdr/95FDEA01463.md): Floorbeam · corroded · Sep 29, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION TOP SIDE OF FLOORBEAM STA 312 LBL 35. REPAIR PER SRM 53-10-2.
- [SDR 95FDEA01462](https://openairdocs.org/sdr/95FDEA01462.md): Stringer · damaged · Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > FASTENERS PULLED THROUGH SIDE OF STR 24R STA 460 TO 484. REMOVED FASTENERS AND REPAIRED STR PER SRM 51-10-3.
- [SDR 95FDEA01461](https://openairdocs.org/sdr/95FDEA01461.md): Skin · corroded · Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > CORROSION BETWEEN SKINS IN CORNER OF FWD ENTRY DOOR CUTOUT, FWD UPPER CORNER APPROX STA 310 TO 318, CORNER OF DOOR AND PROCEEDS FWD TO APPROX STA 303 AREA. REPAIRED PER EA 7-5330-25765 DATED 9-18-95.
- [SDR 95FDEA01455](https://openairdocs.org/sdr/95FDEA01455.md): Casting · corroded · Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > THE 9G NET CASTING HAS HEAVY CORROSION, JUST I/B OF RBL 45 SEAT TRACK AND CRACKED STA 460 TO 487. FABRICATED NEW SUPPORT PER EA 7-5320-25815 DATED 9-25-95. INSTALLED FITTING 9G AT RBL 45 IAW ESO 11782 DATED 9-15-95 AND SRM 51-10-1.
- [SDR 95FDEA01454](https://openairdocs.org/sdr/95FDEA01454.md): Casting · corroded · Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > UPPER LOBE FLOOR, FOUND CORROSION ON 9G NET FLOOR ANCHOR STA 360 LT LBL 24. INSTALLED NEW NET ANCHOR CASTING PER SRM 51-10-1 EA 7-5320-25815 DATED 9-25-95.
- [SDR 95FDEA01453](https://openairdocs.org/sdr/95FDEA01453.md): Skin · cracked · Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT FWD EDGE OF ENTRY DOOR CUTOUT JUST BELOW STR 7L. REPAIRED PER ESO 11782 DATED 9-15-95 AND EA 7-5330-25765 DATED 9-18-95.
- [SDR 95FDEA01456](https://openairdocs.org/sdr/95FDEA01456.md): Frame · cracked · Sep 27, 1995 · N135FE · Boeing 72725C · Fuselage Main, Frame
  > BS 870 TERMINAL FITTING AFT ROW 2ND FASTENER HOLE ABOVE STR 10R HAS CRACK IND, AT 12 O'CLOCK ON O/B SIDE OF O/B FLANGE, RT SIDE FUSELAGE. CRACK IN FRAME STA 870 RT JUST ABOVE STR 10R CRACK IND IS BETWEEN THE 3RD AND 4TH FASTENER ABOVE STR 10R. INSTALLED DOUB
- [SDR 95FDEA01484](https://openairdocs.org/sdr/95FDEA01484.md): Skin · mismfg · Sep 26, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > AFT CARGO BELLY SKIN AT STA 1150, STA 29 - 2 EA HOLES HAVE 2 FASTENERS IN ONE HOLE. REMOVED DAMAGED FASTENERS, INSTALLED DOUBLER ON SKIN PER SRM 53-30-3.
- [SDR 95FDEA01483](https://openairdocs.org/sdr/95FDEA01483.md): Skin · mismfg · Sep 26, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > TWO FASTENERS INSTALLED IN ONE HOLE, THROUGH SHEAR TIE STA 1130, O/B OF STR 29L. REMOVED DAMAGE FROM FASTENERS AT STA 1130 O/B OF STR 29L. INSTALLED DOUBLER OF AFT FUSE BELLY SKIN PER SRM 53-30-3.
- [SDR 95FDEA01431](https://openairdocs.org/sdr/95FDEA01431.md): Floor Beam · corroded · Sep 26, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION OF FLOOR TRACK AT LBL 45 AT BS 360, 400-420 AND 380. REMOVED SECTION OF FLOOR BEAM STATION 360 - 420 AND INSTALLED NEW FLOOR TRACK FROM STA 360-420 PER SRM 51-10-5.
- [SDR 95FDEA01481](https://openairdocs.org/sdr/95FDEA01481.md): Floor Beam · corroded · Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > STA 640, RBL 5 UPPER FLANGE OF FLOOR BEAM HAS EXFOLIATION CORROSION PILLOWED AND BLOWN OUT - REMOVED CORROSION AND INSTALLED DOUBLER REPAIR WITH 7075-T6 EXTRUSIONS AND A 15-5 STAINLESS STEEL STRAP, CAD PLOTED AND HEAT TREATED TO 180-200 RSI, TREATED AND PRIMED
- [SDR 95FDEA01480](https://openairdocs.org/sdr/95FDEA01480.md): Floor Beam · corroded · Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION BOTTOM OF FLOOR BEAM JUST I/B OF RBL 25 SEAT TRACK STA 480. REMOVED PORTION OF CORRODED BEAM - FABRICATED AND INSTALLED DOUBLER PER 53-10-8 FIG 5 OF SRM.
- [SDR 95FDEA01460](https://openairdocs.org/sdr/95FDEA01460.md): Floorbeam · corroded · Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > UPPER LOBE FLOOR, CORROSION ON UNDERSIDE OF FLOORBEAM LT STA 480 BETWEEN BL 0 AND LBL 24. CORROSION REMOVAL WAS BEYOND LIMITS. INSTALLED REPAIR IAW 53-10-8 FIG 5 AND 51-40-2.
- [SDR 95FDEA01459](https://openairdocs.org/sdr/95FDEA01459.md): Flange · corroded · Sep 25, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > UPPER MAIN CARGO, CORROSION ON BOTTOM SIDE OF THE FWD FLANGE STA 480 RBL 5. REMOVED CORROSION AT LOCATIONS PER SRM 51-10-01, INSTALLED REPAIR IAW SRM 53-10-8 FIG 5 AND 51-40-2.
- [SDR 95FDEA01479](https://openairdocs.org/sdr/95FDEA01479.md): Blkhd Web · corroded · Sep 23, 1995 · N135FE · Boeing 72723 · Fuselage Main, Bulkhead
  > AFT CARGO COMP FS 950 BLKD UPPER FLANGE AND WEB CORRODED BETWEEN RBL 24 - 54. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 FIG 2, SRM 51-10-9.
- [SDR 95FDEA01478](https://openairdocs.org/sdr/95FDEA01478.md): Floor Beam · corroded · Sep 23, 1995 · N135FE · Boeing 72723 · Fuselage Main, Floor Beam
  > UPPER LOBE FLOOR STA 480 LT CORROSION ON UNDERSIDE OF FLOOR BEAM BETWEEN LBL 24 AND LBL 45 AROUND FASTENER HOLES. REMOVED CORROSION NR 7 ABOVE LOCATION PER SRM 51-10-06. CORROSION REMOVED BEYOND LIMITS, REPAIRED CORRODED FLOOR BEAM PER 53-10-8 FIG 5.
- [SDR 95FDEA01430](https://openairdocs.org/sdr/95FDEA01430.md): Floor Beam · corroded · Sep 23, 1995 · N135FE · Boeing 72723 · Fuselage Main, Floor Beam
  > HEAVY CORROSION AT F/B SCREW HOLES STA 400, LBL 35 ON FLOOR BEAM TOP SIDE. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA PER SRM 53-10-8. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8, PG 45 - 48.
- [SDR 95FDEA01477](https://openairdocs.org/sdr/95FDEA01477.md): Spar · corroded · Sep 21, 1995 · N135FE · Boeing 72725C · Wing Spar
  > RIVET HEAD POPPED AND CORROSION ON OUTSIDE OF CENTER TANK REAR SPAR JUST FWD OF STA 870 RT, RBL 50. REMOVED CORR - MATERIAL THICKNESS BEYOND MM LIMIT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AA ESO 11782. AWAITING FEDEX EA.
- [SDR 95FDEA01398](https://openairdocs.org/sdr/95FDEA01398.md): Floor Beam · corroded · Sep 19, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > ON NR 0234, CORROSION ON FLOOR BEAM IN MAIN CARGO STA 420 RBL 20. CORROSION REMOVED BEYOND LIMITS. CUT OUT AREA AND INSTALLED.090 INCH DOUBLERS AND FILLER PER SRM 53-11-8, FIG 8.
- [SDR 95FDEA01397](https://openairdocs.org/sdr/95FDEA01397.md): Rib · cracked · Sep 18, 1995 · N135FE · Boeing 72725C · Rudder, Spar/Rib
  > UPPER RUDDER THRUST HINGE, LOWER LT SIDE. RIB IS CRACKED BETWEEN FASTENERS. REMOVED 6 EACH FASTENERS - HFEC CHECKED. VERIFIED CRACK FROM HOLE-TO-HOLE, AFT ROW. INSTALLED DOUBLER PER FEDEX EA 7-5510-25773 DATED 9-15-95. PAINTED ALL AREAS EFFECTED FOR WATER-
- [SDR 95FDEA01387](https://openairdocs.org/sdr/95FDEA01387.md): Aft Trunnion · damaged · Sep 18, 1995 · N135FE · Boeing 72725C · Fuselage, Landing Gear Attach Fittings
  > LEFT WING FRONT SPAR FORWARD TERMINAL PIN JOINT HOLE CRACKED AFT FORWARD. LEVELED AND SHORED A/C IAW SRM 51-50-1. CUT LOWER CHORD ANGLE AND WEB IAW BOEING DWG 65C29064. REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER C
- [SDR 95FDEA01366](https://openairdocs.org/sdr/95FDEA01366.md): Floor · damaged · Sep 18, 1995 · N135FE · Boeing 72725C · Fuselage Floor Panel
  > UNAUTHORIZED REPAIR INSTALL ON FLOOR, BS 344 LBL 38. REMOVED AND REPLACED REPAIR PER DRAWING NR SR27-53-007, NR O857.
- [SDR 95FDEA01369](https://openairdocs.org/sdr/95FDEA01369.md): Floorbeam · corroded · Sep 16, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION ON MAIN CABIN FLOORBEAM STA 400 AT LBL 35.
- [SDR 95FDEA01396](https://openairdocs.org/sdr/95FDEA01396.md): Skin · damaged · Sep 15, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > STR 9R HAD HOLE AND CRACK AND ONE FAST HOLE WITH EXISTING MISDRILL CAUSED DAMAGE IN FUSELAGE SKIN (A/C CAME IN WITH THIS COND). STR DAMAGE AND FUSELAGE SKIN DAMAGE WAS CUT OUT AND STR SPLICE 9.050 INCH DOUBLER ON SKIN WAS INSTALLED, PER SRM 53-30-3, FIG 9, N

Next page: https://openairdocs.org/deregistered/N135FE-2004-08-26/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 = 'N135FE' AND deregistration_id = 'N135FE-2004-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N135FE-2004-08-26/reports

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