# Service difficulty reports: N269FE, cancelled Aug 22, 2014

A list on [N269FE, cancelled Aug 22, 2014](https://openairdocs.org/deregistered/N269FE-2014-08-22.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 · 82 reports

- [SDR FDEA201206212285](https://openairdocs.org/sdr/FDEA201206212285.md): Seal · failed · Jun 21, 2012 · N269FE · Boeing 727233 · Passenger/Crew Doors
  > AIRPLANE COULD ONLY HOLD STABLE CABIN PRESSURE UP TO 24,000 FT WITH AUTO PRESSURE CONTROLLER SET AT 24,000 FT, CABIN ALTITUDE SHOULD HAVE BEEN 1,000 FT BUT WAS 6,100 FT WITH A 6.2 DIFFERENTIAL AND CARGO HEAT OUTFLOW VALVE CLOSED. PERFORMED PRESSURIZATION CH
- [SDR FDEA201205221933](https://openairdocs.org/sdr/FDEA201205221933.md): Unknown · unknown · May 22, 2012 · N269FE · Boeing 727233 · Cabin Pressure Control System
  > PRESSURIZATION SYS NOT FUNCTIONING PROPERLY. COULD NOT GET MORE THAN 6.0 PSID, 9600FT CABIN ALT AND SLOWLY CLIMBING AT FL330. DECENDED TO FL270, DIFFERENTIAL REDUCED TO 5.0 PSI CARGO HEAT VALVE CLOSED FULL TIME AT 10,000FT, CABIN ALT= 5500, DIFFERENTIAL 1
- [SDR FDEA201108043091](https://openairdocs.org/sdr/FDEA201108043091.md): Skin · corroded · Aug 4, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD PIT, REMOVED SOFT SEALANT BTW BS 720C - 720D BTW STR 28L - STR 28R EVIDENCE OF CORROSION. REMOVED CORROSION ON SKIN IAW B727 SRM 51-10-6. ORIGINAL MAT. 0.072", REMAINING MAT. 0.054", MAT. LOSS 0.018". FOUND TO BE WITHIN LIMITS IAW EA 7-5330-136797.
- [SDR FDEA201108023094](https://openairdocs.org/sdr/FDEA201108023094.md): Skin · misrepaired · Aug 2, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS FASTENERS WITH IMPROPER SPACING, STA 420-440 BELOW STR 4L. TRIMMED UPPER AND LOWER SKIN AREA BETWEEN STA 420 TO STA 440, STR 4L, FABRICATED FREEZE PLUGS, DOUBLER, FILLER, TAPERED FILLER, TWO FILLER INTERNAL SKIN AND INSTALLED REPAIR PART
- [SDR FDEA201108023077](https://openairdocs.org/sdr/FDEA201108023077.md): Skin · corroded · Aug 2, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT BS 720B, 18" STR 27L HAS EXFOLIATION. CUT OUT DAMAGED AREA OF SKIN, FABRICATED REPAIR DOUBLER AND NEW TEE SUPPORT, AND INSTALLED NEW TEE SUPPORT AND DOUBLER IAW EA 7-5330-136797.
- [SDR FDEA201108023093](https://openairdocs.org/sdr/FDEA201108023093.md): Skin · misrepaired · Aug 2, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS FASTENERS WITH IMPROPER SPACING, STA 440-460 BELOW STR 4L. TRIMMED UPPER AND LOWER SKIN AREA BETWEEN STA 440 TO STA 460, STR 4L, FABRICATED DOUBLER, FILLER, TWO FILLER INTERNAL SKIN AND INSTALLED REPAIR PARTS IAW EA 7-5330-136790.
- [SDR FDEA201108013059](https://openairdocs.org/sdr/FDEA201108013059.md): Support Angle · corroded · Aug 1, 2011 · N269FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD PIT BS 740 LOWER SUPPORT ANGLE HAS CORROSION, LOWER SURFACE AFT OF STR 27L. REMOVED AND REPLACED SUPPORT ANGLE AT BS 740 IAW SRM 51-30-5 AND 51-30-2 REV 103 AND DWG 69-43695.
- [SDR FDEA201107313045](https://openairdocs.org/sdr/FDEA201107313045.md): Seat Track · corroded · Jul 31, 2011 · N269FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 760-848, RBL 45.5. REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED SEAT TRACK IAW SRM 51-10-6, 53-10-1 FIG 3, 51-10-2, 53-10-5 FIG 2 AND 51-30-2.
- [SDR FDEA201107262944](https://openairdocs.org/sdr/FDEA201107262944.md): Shear Tie · corroded · Jul 26, 2011 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FWD PIT FRAME, BS 720C, AFT SHEAR TIE IS CORRODED BETWEEN STRINGERS 26-27R. REMOVED SHEAR TIE IAW SRM 51-30-2. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-30-2. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2, REV 103.
- [SDR FDEA201107222890](https://openairdocs.org/sdr/FDEA201107222890.md): Support Angle · corroded · Jul 22, 2011 · N269FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > BS 740 ANGLE IS CORRODED WITH EXFOLIATION BETWEEN STRINGER 28R AND 27R. REMOVED SUPPORT ANGLE IAW SRM 51-30-2 REV 103. FABRICATED NEW ANGLE IAW SRM 51-20-1 FIG 7 AND 51-30-5. INSTALLED SUPPORT ANGLE IAW SRM 51-30-2 AND DWG 69-64841
- [SDR FDEA201107212871](https://openairdocs.org/sdr/FDEA201107212871.md): Shear Tie · corroded · Jul 21, 2011 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 700, INBD OF STRINGER 28L. CUT OUT DAMAGED SHEAR TIE IAW SRM 51-10-1. FABRICATED SHEAR TIE DOUBLER IAW SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE REPAIR DOUBLER IAW SRM 53-10-4 FIG 15 REV 103.
- [SDR FDEA201107192811](https://openairdocs.org/sdr/FDEA201107192811.md): Spar · cracked · Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Frame
  > CENTER TANK REAR SPAR UPPER WEB BL 0 TO LBL 2 HAS UT SHEAR WAVE CRACK INDICATION AND BL 0 TO RBL HAS HFEC CRACK INDICATION. STOP DRILLED HOLES AT CENTER TANK REAR SPAR UPPER WEB LBL 0-2 AND RBL 0-2 IAW SRM 51-10-1. LOCATED AND DRILLED HOLES AT REPAIR KIT AND
- [SDR FDEA201107192810](https://openairdocs.org/sdr/FDEA201107192810.md): Skin · gouged · Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620, STR 8L. REMOVED DAMAGED INNER SKIN, FABRICATED AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2. FIG 3A AND SRM 51-30-2.
- [SDR FDEA201107192809](https://openairdocs.org/sdr/FDEA201107192809.md): Skin · corroded · Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > SKIN BULGE STA 440, STR 20R. CUTOUT DAMAGED SKIN -DAMAGED AREA, FABRICATED REPAIR SKIN, REINFORCING STRAPS, SPLICE PLATE AND TAPERED FILLER AND INSTALLED REPAIR SKIN, REINFORCING STRAPS, SPLICE PLATE AND TAPERED FILLER IAW SRM 53-30-3 FIG 12.
- [SDR FDEA201107152717](https://openairdocs.org/sdr/FDEA201107152717.md): Torque Box · cracked · Jul 15, 2011 · N269FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIR AREA - LIGHTNING HOLE IS CRACKED AT RT LOWER TORQUE BOX BS 1223. CUT OUT DAMAGED WEB IAW SRM 51-10-1 REV 103. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND SRM 51-40-2.
- [SDR FDEA201107152716](https://openairdocs.org/sdr/FDEA201107152716.md): Torque Box · cracked · Jul 15, 2011 · N269FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIR AREA - LIGHTNING HOLE IS CRACKED AT RT LOWER TORQUE BOX BS 1233. CUT OUT DAMAGED WEB IAW SRM 51-10-1 REV 103. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2
- [SDR FDEA200907142620](https://openairdocs.org/sdr/FDEA200907142620.md): Accessory Unit · failed · Jul 14, 2009 · N269FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF, THE LANDING GEAR LEVER LATCH FAILED TO RELEASE. LANDING GEAR LEVER COULD ONLY BE RAISED TO OFF POSITION. HORN SOUNDED WHEN FLAPS RETRACTED FROM 5 DEG. TO 2 DEG. REMOVED AND REPLACED M831 AIR SENSING SENSOR PER AMM 32-09-221-4 AND PERFORM
- [SDR FDEA200902120510](https://openairdocs.org/sdr/FDEA200902120510.md): Door Frame · cracked · Feb 12, 2009 · N269FE · Boeing 727233 · Fuselage Main, Structure
  > CORRECTION OF SDR 09-0481 FWD CARGO DOORWAY STA 620 LOWER INNER CHORD CRACKED. FABRICATED CHORD ON MAE TRAVELER T9/778261. FABRICATED SPLICE ON MAE TRAVELER T9/779262. CHORD REMOVED AND NEW INSTALLED IAW SRM 51-30-2 AND SRM 51-40-4. MAJOR REPAIR, RII, RD
- [SDR FDEA200902090484](https://openairdocs.org/sdr/FDEA200902090484.md): Stringer · corroded · Feb 9, 2009 · N269FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD CARGO AREA BS 720F TO 740 S-26L STRINGER SEVERAL ROW OF RIVETS CORRODED REPAIRED STRINGER IAW SRM 53-10-3. FABRICATED STRINGER ON MAE TRAVILER T9/778825. MAJOR REPAIR, RII, RDR AND SDR.
- [SDR FDEA200902070482](https://openairdocs.org/sdr/FDEA200902070482.md): Seat Track · corroded · Feb 7, 2009 · N269FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MCD SEAT TRACK FLANGE HAS CORROSION AT LBL24 APPROX FROM STA 370 TO 460. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. FABRICATED TRACK AND SPLICES ON MAE TRAVELER T9/779235 AND T9/779236. MAJOR REPAIR, RII, RDR AND SDR.
- [SDR FDEA200902070481](https://openairdocs.org/sdr/FDEA200902070481.md): Structure · cracked · Feb 7, 2009 · N269FE · Boeing 727233 · Fuselage Main, Structure
  > FWD CARGO DOORWAY STA 620 LOWER INNER CHORD CRACKED. FABRICATED CHORD ON MAE TRAVELER T9/778261. FABRICATED SPLICE ON MAE TRAVELER T9/779262. REPAIRED CHORD IAW SRM 53-10-2. MAJOR REPAIR, RII, RDR AND SDR.
- [SDR 07FDEA00910](https://openairdocs.org/sdr/07FDEA00910.md): Door · unsecure · Mar 15, 2007 · N269FE · Boeing 727233 · Passenger/Crew Doors
  > AFTER TAKEOFF IN IAD CABIN ALTITUDE WENT ABOVE 10,00 0' RAN QRH PROCEDURES CABIN ALTITUDE WENT TO 11,500' WENT ON O2 RETURNED TO IAD. NOTICE FORWARD ENTRY DOOR WAS NOT SEATED PROPERLY OPEN AND SECURED DOOR SEVERAL TIMES, PERFORMED FORWARD ENTRY DOOR INSPECT
- [SDR 06FDEA03917](https://openairdocs.org/sdr/06FDEA03917.md): Friction Brake · out of adjust · Nov 8, 2006 · N269FE · Boeing 727233 · Power Lever
  > ON T/O AND CLIMB NR 2 THROTTLE CONSTANTLY CREEPS FORWARD 3-4% N1. THROTTLE NEEDS TO BE CONSTANTLY PULLED BACK NOT TO OVERSPEED ENGINE. ADJUSTED NR 2 ENG FRICTION BRAKE PER 727-200 M/M 76-11-001-8. OPS CHECKED NORMAL.
- [SDR 06FDEA03577](https://openairdocs.org/sdr/06FDEA03577.md): Throttle · unknown · Oct 3, 2006 · N269FE · Boeing 727233 · Power Lever
  > AFTER LEVEL OFF AT FL 320, F/O NOTED THE NR 2 THROTTLE MOVED ITSELF TO FIREWALL POWER WHILE THROTTLES 1 AND 3 REMAINED AT CLIMB POWER. IMMEDIATELY RETARDED THE THROTTLE BACK TO MATCH 1 AND 3. EPR ON NR 2 WAS 2.57 AND TEMP EXCEEDED 650 DEG. OVERBOOST APPROX
- [SDR 06FDEA2315](https://openairdocs.org/sdr/06FDEA2315.md): Attach Fitting · corroded · Jun 15, 2006 · N269FE · Boeing 727200 · Trailing Edge Flaps
  > CORROSION ON FWD ATTACH FITTING AT NR 3 FLAP TRACK.
- [SDR 06FDEA2256](https://openairdocs.org/sdr/06FDEA2256.md): Frame · misdrilled · Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, Frame
  > DOUBLE HOLE AT BS 600 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.
- [SDR 06FDEA2255](https://openairdocs.org/sdr/06FDEA2255.md): Frame · misdrilled · Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, Frame
  > DOUBLE HOLE AT BS 520 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.
- [SDR 06FDEA2254](https://openairdocs.org/sdr/06FDEA2254.md): Frame · misdrilled · Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, Frame
  > DOUBLE HOLE AT BS 500 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.
- [SDR 06FDEA2247](https://openairdocs.org/sdr/06FDEA2247.md): Beam · corroded · Jun 7, 2006 · N269FE · Boeing 727200 · Spoilers
  > WHILE WORKING CARD N00862, FOUND CORROSION AT WBL 206, LOWER CHORD OF SPOILER BEAM LOWER SURFACE, RIGHT WING. *S/D* REPAIRED CORROSION RIGHT WING LOWER CHORD OF SPOILER BEAM LWR SURFACE AT WBL 206 IAW FED EX EA 7-5710-100546.
- [SDR 06FDEA2246](https://openairdocs.org/sdr/06FDEA2246.md): Web · misdrilled · Jun 7, 2006 · N269FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > WHILE WORKING CUST CARD N00346 FOUND LOWER SIDE OF THE FLOOR WEB AT BS 1175 RBL 26 WL 208 FASTENER HOLES -SNOWMANNED-. REPAIRED FLOOR WEB AT BS 1175, RBL 26, WL 208 IAW SRM 53-10-1 FIG 1.
- [SDR 06FDEA2248](https://openairdocs.org/sdr/06FDEA2248.md): Skin · dented · Jun 7, 2006 · N269FE · Boeing 727200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR EXTERNAL SKIN DENTED 20 INCHES FROM AFT EDGE AND 47 INCHES FROM BOTTOM EDGE. REPAIRED DENT PER FED EX EA 7-5230-102256.
- [SDR 06FDEA2220](https://openairdocs.org/sdr/06FDEA2220.md): Strap · corroded · Jun 6, 2006 · N269FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > BS 950E STR 29 RT IS CORRODED. FOUND CORROSION TO BE ON REPAIR STRAP, REMOVED AND REPLACED REPAIR STRAP BS 950E STR 29R IAW SRM 51-30-2 AND FED EX DWG SR27-53-023 REV A.
- [SDR 06FDEA2219](https://openairdocs.org/sdr/06FDEA2219.md): Repair · damaged · Jun 6, 2006 · N269FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR 12" X 37" ON LOWER FUSELAGE BETWEEN BS 680-BS 690 STR 26L-27R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPAIRED DOUBLER AT BS 680 TO BS 720, STR 26L TO S
- [SDR 06FDEA2183](https://openairdocs.org/sdr/06FDEA2183.md): Repair · misinstalled · Jun 1, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL REPAIR DOUBLER 22" BY 16" BS 700 STR 27L - 28R IS NOT PER SRM. REMOVED AND REPLACED DOUBLER AT BS 700 STR 27L TO STR 28R IAW SRM 53-30-3.
- [SDR 06FDEA2182](https://openairdocs.org/sdr/06FDEA2182.md): Repair · misinstalled · Jun 1, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL REPAIR DOUBLER 11" BY 17" ON LOWER FUSELAGE BS 720 STA 28L -28R IS NOT PER SRM. REMOVED AND REPAIRED DOUBLER BS 720 STR 28L TO 28R IAW SRM 53-30-3.
- [SDR 06FDEA2124](https://openairdocs.org/sdr/06FDEA2124.md): Shear Tie · corroded · May 31, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FOUND BS 1110 BETWEEN STRS 30 AND 29 RT SHEAR TIE IS CORRODED. REPAIRED SHEAR TIE IN AFT CARGO BAY AT BS 1110 BETWEEN S30 & 29R IAW SRM 51-40-03.
- [SDR 06FDEA2058](https://openairdocs.org/sdr/06FDEA2058.md): Shear Tie · corroded · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE AT BS 720, STRINGER 28 LT TO 28 RT CORRODED. REMOVED CORRODED SHEAR TIE AT BS 720 STR 28 RT - 28 LT, FORMED NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.
- [SDR 06FDEA2056](https://openairdocs.org/sdr/06FDEA2056.md): Shear Tie · corroded · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE AT BS 700 STRINGER 28 LT TO 28 RT CORRODED. REMOVED CORRODED SHEAR TIE STR 28 LT - 28 RT BS 700, FORMED NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-4.
- [SDR 06FDEA2061](https://openairdocs.org/sdr/06FDEA2061.md): Doubler · improper · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR 8" BY 14" ON LOWER FUSELAGE BS 1166, STR 19L-20L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED LOWER FUSELAGE SKIN REPAIR DOUBLER BS 1166 STR 19
- [SDR 06FDEA2060](https://openairdocs.org/sdr/06FDEA2060.md): Doubler · improper · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR 7" BY 7" ON LT SIDE OF FUSELAGE AFT OF MLG WHEEL WELL AT BS 950A, STR 25L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER, FABRICATED, DRILLED, TRI
- [SDR 06FDEA2059](https://openairdocs.org/sdr/06FDEA2059.md): Doubler · improper · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR 5" BY 18" ON LOWER FUSELAGE BS 1243, STR 22R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INVESTIGATED REPAIR AT BS 1243 STR 22R, FOUND NOT TO BE PER APPROVED DATA.
- [SDR 06FDEA2055](https://openairdocs.org/sdr/06FDEA2055.md): Repair · improper · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR 14" BY 16" ON LOWER FUSELAGE CENTERLINE AT BS 660, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR IS NOT PER SRM, REMOVED EXISTING REPAIR, FABRICATED AND
- [SDR 06FDEA2057](https://openairdocs.org/sdr/06FDEA2057.md): Shear Tie · corroded · May 29, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE AT BS 700 STRINGER 27 LT TO 28 LT CORRODED. REMOVED CORRODED SHEAR TIE STR 27 LT - 28 LT. FORMED NEW SHEAR TIE & INSTALLED IAW SRM 53-10-4.
- [SDR 06FDEA2039](https://openairdocs.org/sdr/06FDEA2039.md): Stringer · corroded · May 26, 2006 · N269FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 28 LT TO BE CORRODED AT BS 680-700. REMOVED S28R AND PRODUCTION SPLICES BS 680-700 AND REINSTALLED NEW STRINGER IAW FED EX SRM 51-30-2.
- [SDR 06FDEA2038](https://openairdocs.org/sdr/06FDEA2038.md): Stringer · corroded · May 26, 2006 · N269FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 28 RT TO BE CORRODED AT BS 680-700. REMOVED S28R BS 680-700 RT & PRODUCTION SPLICES AND REINSTALLED NEW STRINGER PER FED EX SRM 51-30-2.
- [SDR 06FDEA2037](https://openairdocs.org/sdr/06FDEA2037.md): Flap Track · corroded · May 26, 2006 · N269FE · Boeing 727233 · Trailing Edge Flaps
  > FOUND CORROSION ON NR 6 FLAP TRACK AFT MOUNT PAD. REMOVED AND REPLACED NR 6 FLAP TRACK IAW TASK CARD 27X5708-03.
- [SDR 06FDEA2028](https://openairdocs.org/sdr/06FDEA2028.md): Flap Track · corroded · May 26, 2006 · N269FE · Boeing 727233 · Trailing Edge Flaps
  > NR 3 FLAP TRACK UPPER SURFACE CORRODED FWD ATTACH PT OB HOLE. REMOVED AND REPLACED NR 3 FLAP TRACK IAW TASK CARD 27X5705-03.
- [SDR 06FDEA2029](https://openairdocs.org/sdr/06FDEA2029.md): Floorbeam · corroded · May 26, 2006 · N269FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FOUND BS 1130 FLOORBEAM TO BE CORRODED AT RBL 7 TO RBL 9 WL 208. REPAIRED BS 1130 FLOOR BEAM RBL 7 - 9 IAW SRM 53-10-8 FIG 11 DETAIL II.
- [SDR 06FDEA2002](https://openairdocs.org/sdr/06FDEA2002.md): Spacer · loose · May 24, 2006 · N269FE · Boeing 727233 · Elevator Structure
  > RIGHT ELEVATOR, NR 1 ELEVATOR RUB BLOCK SPACER IS LOOSE IN LOWER TRAILING EDGE BEAM. REPAIRED R/H ELEVATOR NR 1 RUB BLOCK SPACER IN T/E BEAM IAW FED-EX EA 7-5510-100547.
- [SDR 06FDEA1980](https://openairdocs.org/sdr/06FDEA1980.md): Shear Tie · corroded · May 22, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FOUND BS 1148 BETWEEN STRS 30 AND 29 RT SHEAR TIE IS CORRODED. REMOVED SHEAR TIE BS 1148 STR 29 & 30 R/H PER SRM 51-30-2. BLENDED CORROSION 3 X 3.030. ORIG THICKNESS.063. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SHEAR TIE USING 7075T6.063 LOT #500810

Next page: https://openairdocs.org/deregistered/N269FE-2014-08-22/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 = 'N269FE' AND deregistration_id = 'N269FE-2014-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N269FE-2014-08-22/reports

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