# Service difficulty reports: N270FE, cancelled Dec 17, 2008

A list on [N270FE, cancelled Dec 17, 2008](https://openairdocs.org/deregistered/N270FE-2008-12-17.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 · 94 reports

- [SDR 08FDEA04355](https://openairdocs.org/sdr/08FDEA04355.md): Stringer Clip · cracked · Oct 15, 2008 · N270FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > MAIN CABIN UPPER LOBE STA 680 STR 4L CLIP CRACKED REMOVED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. INSTALLED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA04354](https://openairdocs.org/sdr/08FDEA04354.md): Stringer Clip · corroded · Oct 15, 2008 · N270FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FWD PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 700, STR 26L, WL 153. REMOVED STRINGER CLIP, CORROSION ON CLIP WAS EXFOLIATED BEYOND REPAIR. FABRICATED, TREATED, AND PRIMED NEW CLIP, P/N 69-47375-2. INSTALLED CLIP REF SRM 51-30-2, PG 1-4/BOEING DWG NR 69-4
- [SDR 07FDEA04686](https://openairdocs.org/sdr/07FDEA04686.md): Switch · failed · Oct 25, 2007 · N270FE · Boeing 727233 · Leading Edge Slat Control System
  > ON FLAP RETRACTION TO 2 DEGREES, NR 2 LE FLAP REMAINS EXTENDED. NORMAL HYDRAULICS. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES IAW QRH. NO LUCK. NO ASYMMETRIC CONTROL FORCES NOTED. OBTAINED NORMAL FLAPS 30 LANDING CONFIGURATION. REMOVED AND REPLACED NR
- [SDR 07FDEA03586](https://openairdocs.org/sdr/07FDEA03586.md): Valve · leaking · Sep 11, 2007 · N270FE · Boeing 727233 · Master Cylinder/Brake Valve
  > CALLED BACK BY RAMP. MX NOTICED HYD LEAK/PUDDLE ON GND AFTER WE TOOK OFF. REPLACED NR 3 BRAKE SHUTTLE VALVE PER B727 AMM 32-41-051-4. LK CKS GOOD.
- [SDR 07FDEA02367](https://openairdocs.org/sdr/07FDEA02367.md): Control Knob · misaligned · Jul 3, 2007 · N270FE · Boeing 727233 · Fuel Quantity Indicator
  > CLIMBING THRU 10,000' NOTICED NR 3 FUEL TANK SHOWED HAVING ALL IT'S FUEL AND NR 2 SHOWED HAVING BURNED TWICE THE AMOUNT IT SHOULD HAVE. AFTER FURTHER ANALYSIS CONCLUDED THE NR 3 CROSSFEED VALVE WAS NOT OPERATING AS THE INDICATOR SWITCH WAS SHOWING. WHEN THE
- [SDR 06FDEA1959](https://openairdocs.org/sdr/06FDEA1959.md): Repair · unknown · May 18, 2006 · N270FE · Boeing 72722 · Wing Main, Frame Structure
  > FOUND PREVIOUSLY REPAIR ON LT INBD MID FLAP LOWER SURFACE INBD OF INBD CARRIAGE FAIRING IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR PARTS IAW EA 7-5710-92428. REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.
- [SDR 06FDEA1786](https://openairdocs.org/sdr/06FDEA1786.md): None · none · May 11, 2006 · N270FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT LT ELEVATOR INBOARD UPPER SURFACE WAS ACCOMPLISHED IAW SRM 55-20-3 FIG 1 PAGE 1, BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANS
- [SDR 06FDEA1784](https://openairdocs.org/sdr/06FDEA1784.md): Repair · misinstalled · May 11, 2006 · N270FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FOUND EXISTING REPAIR INSTALLED AT STA 270 STR 17L IS NOT CONFORMED TO FAA APPROVED REPAIR DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3A. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND SRM 53-30-3 FIG 3A. REPAIR IS CLASSIF
- [SDR 06FDEA1783](https://openairdocs.org/sdr/06FDEA1783.md): Repair · misinstalled · May 11, 2006 · N270FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 280 STR 22R IS NOT CONFORMED TO FAA APPROVED REPAIR DATA. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 4. INSTALLED REPAIR DOUBLER IAW SRM 53-30-2 AND SRM 53-30-3. REPAIR IS CLASSIFIED A
- [SDR 06FDEA1753](https://openairdocs.org/sdr/06FDEA1753.md): Repair · misinstalled · May 9, 2006 · N270FE · Boeing 727233 · Fuselage Main, Structure
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 765 STR 8R IS NOT CONFORMED TO FAA APPROVED DATA, REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6- 2-100.
- [SDR 06FDEA1745](https://openairdocs.org/sdr/06FDEA1745.md): Repair · misinstalled · May 8, 2006 · N270FE · Boeing 727233 · Leading Edge Devices
  > FOUND PREVIOUSLY REPAIR INSTALLED ON NR 7 LEADING EDGE SLAT IS NOT COMPLIED WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER IAW SRM 57-50-3, FIG 1. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
- [SDR 06FDEA1722](https://openairdocs.org/sdr/06FDEA1722.md): None · none · May 5, 2006 · N270FE · Boeing 727233 · Standard Practices/Structures
  > PREVIOUSLY REPAIR INSTALLED AT STA 710, STR 21L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 2 PAGE 9. BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS.
- [SDR 06FDEA1721](https://openairdocs.org/sdr/06FDEA1721.md): None · none · May 5, 2006 · N270FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT LT FWD ENTRY DOOR HINGE CUTOUTS WAS ACCOMPLISHED IAW EA 7-5330-28325, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP
- [SDR 06FDEA1706](https://openairdocs.org/sdr/06FDEA1706.md): None · none · May 5, 2006 · N270FE · Boeing 727200 · Standard Practices/Structures
  > FOUND REPAIR LOCATED AT STA 410 STR 15 RT, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INS
- [SDR 06FDEA1707](https://openairdocs.org/sdr/06FDEA1707.md): None · none · May 5, 2006 · N270FE · Boeing 727200 · Standard Practices/Structures
  > FOUND REPAIR LOCATED AT STA 203 STR 28R REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRIT
- [SDR 06FDEA1708](https://openairdocs.org/sdr/06FDEA1708.md): None · none · May 5, 2006 · N270FE · Boeing 727200 · Standard Practices/Structures
  > FOUND REPAIR LOCATED AT STA 1050 STR 29L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 2, REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100
- [SDR 06FDEA1705](https://openairdocs.org/sdr/06FDEA1705.md): None · none · May 4, 2006 · N270FE · Boeing 727233 · Standard Practices/Structures
  > FOUND REPAIR LOCATED ON AFT CARGO DOOR REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DETERMINED TO BE IAW SRM 52-00-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALL
- [SDR 05FDEA00089](https://openairdocs.org/sdr/05FDEA00089.md): Control Unit · contaminated · Jan 13, 2005 · N270FE · Boeing 727200 · Fire Detection
  > CARGO SMOKE IN LOWER, FORWARD CARGO COMPARTMENT. DISCHARGED NR 1 BOTTLE. CARGO SMOKE ON FRONT PANEL AND S/O'S PANEL ILLUMINATED FOR APPROXIMATELY 2 SECONDS. REMOVED AND REPLACED NR 1 LOWER CARGO COMPMENT FIRE BOTTLE, TESTS GOOD. FOUND LOWER CARGO COMPMENT
- [SDR 04FDEA01706](https://openairdocs.org/sdr/04FDEA01706.md): Control Unit · failed · Jun 13, 2004 · N270FE · Boeing 727200 · Fire Detection
  > DISCHARGED BOTH LOWER CARGO COMPT FIRE BOTTLES, INDICATION OF FWD LOWER CARGO FIRE. AFTER CHECKING COMPARTMENT AND WHILE BEING TOWED HAD ANOTHER ACTIVATION OF LOWER CARGO FIRE WARNING. REMOVED AND REPLACED LWR FWD CARGO COMPT FIRE SUPP/SMOKE DET CONTROL ELEC
- [SDR 04FDEA01696](https://openairdocs.org/sdr/04FDEA01696.md): Control Unit · malfunctioned · Jun 11, 2004 · N270FE · Boeing 727200 · Fire Detection
  > FORWARD LOWER CARGO COMPARTMENT FIRE INDICATION ON TAXI OUT. NO ACTUAL FIRE REPORTED BY FIRE DEPARTMENT AFTER FIRE BOTTLES DISCHARGED INTO FWD LOWER CARGO COMPARTMENT. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES AND THE CARTRIDGES PER MM 26-17-014-
- [SDR 04FDEA00379](https://openairdocs.org/sdr/04FDEA00379.md): Warning Horn · false activation · Feb 7, 2004 · N270FE · Boeing 727200 · Fire Detection
  > LOWER CARGO SMOKE WARNING BELL ACTIVATED TWICE AT ALTITUDE FOR 1-2 SECONDS. WARNING LIGHTS AND HORN WENT OUT IMMEDIATELY WITHOUT ACTIVATING THE DISCHARGE BUTTON. BEGAN IMMEDIATE DESCENT INTO YMX. WARNING CAME ON CONTINUOUS AT 500 FT, PUSH BOTTLE DISCHARGE B
- [SDR 03FDEA01906](https://openairdocs.org/sdr/03FDEA01906.md): Attach Angle · corroded · Nov 12, 2003 · N270FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > WHILE WORKING NRC N01585 FOUND CORROSION AT STA 950 10 RBL 11 TO 50 WL 148, RT MLG BANANA FAIRING ATTACH ANGLE. CORROSION AT BS 950 10, RBL 11 TO 50, WL 148 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED REPAIR ANGLES AND FILLERS AND INSTALLED FOR RT
- [SDR 03FDEA01905](https://openairdocs.org/sdr/03FDEA01905.md): Frame · gouged · Nov 11, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > GOUGE ON BS 540 FRAME, I/B FLANGE, ONE INCH ABOVE STR 22L. BLENDED GOUGE AREA ON FRAME AT BS 540 ABOVE STR 22L, 1 X 1 X.008 INCH ORIGINAL THICKNESS.045 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 1 FIG 1, DETAIL I. REMOVED AND REPLACED LOWER LEFT F
- [SDR 03FDEA01903](https://openairdocs.org/sdr/03FDEA01903.md): Keelbeam · corroded · Nov 11, 2003 · N270FE · Boeing 727200 · Fuselage Main, Keel
  > CORRODED KEEL BEAM STR 29L, O/B FLANGE BS 950D - 1004. CORROSION ON KEEL BEAM STR 29L O/B FLANGE BS 950D-1004 REPAIRED PER EA 7-5310- 55109 & SR 27-53-023A.
- [SDR 03FDEA01902](https://openairdocs.org/sdr/03FDEA01902.md): Spar · chafed · Nov 11, 2003 · N270FE · Boeing 727200 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB STRINGER 7 CHAFED UNDER AFT CORNER OF ACCESS PANEL 9601. REPAIRED DAMAGE TO LT VERTICAL FIN MID SPAR AT FIN STA 229 PER SRM 55-30-06 FIGURE 3.
- [SDR 03FDEA01904](https://openairdocs.org/sdr/03FDEA01904.md): Floorbeam · corroded · Nov 11, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-04) BS 1130 FLOORBEAM UPPER CHORD AROUND HOLES AND UNDER NUT PLATES, LBL 48, WL 208.
- [SDR 03FDEA01899](https://openairdocs.org/sdr/03FDEA01899.md): Hinge · corroded · Nov 10, 2003 · N270FE · Boeing 727200 · Landing Gear Doors
  > CORROSION ON FASTENERS ALONG UPPER LT GEAR BODY DOOR HINGE AREA ENTIRE LENGTH. *S/D* CORROSION ALONG UPPER LT GEAR BODY DOOR HINGE AREA ENTIRE LENGTH. ORIG THICKNESS.020. LOWEST READING.078, FOUND TO BE IN LIMITS IAW SRM 53-10-1.
- [SDR 03FDEA01898](https://openairdocs.org/sdr/03FDEA01898.md): Frame · dented · Nov 10, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > FWD LWR CARGO FRAME IS DENTED AT STA 600, STR 24L. REMOVED AND REPLACED DAMAGED FRAME SECTION BS 600, STR 21L TO STR 25L PER SRM 51-30-2.
- [SDR 03FDEA01886](https://openairdocs.org/sdr/03FDEA01886.md): Failsafe · cracked · Nov 7, 2003 · N270FE · Boeing 727200 · Fuselage Main, Structure
  > CRACKED FAILSAFE CHORD, BS 804 AT STR 14L.
- [SDR 03FDEA01887](https://openairdocs.org/sdr/03FDEA01887.md): Floorbeam · corroded · Nov 7, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > WHILE WORKING CARD N01482, FOUND CORROSION ON FLOORBEAM, STA 328 LBL 23 WL 208.
- [SDR 03FDEA01888](https://openairdocs.org/sdr/03FDEA01888.md): Floorbeam · corroded · Nov 7, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > WHILE DRILLING UP NEW SEAT TRACK AT BS 1050 LBL 25 DRILLED THROUGH RADIUS OF FLOORBEAM REPAIR ANGLE.
- [SDR 03FDEA01876](https://openairdocs.org/sdr/03FDEA01876.md): Frame · corroded · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION FOUND ON FORWARD SIDE OF 950E FRAME AT STRINGER 29 LT. REPAIRED PER B727 SRM 53-10-4 FIG 15.
- [SDR 03FDEA01871](https://openairdocs.org/sdr/03FDEA01871.md): Floorbeam · corroded · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > WHILE WORKING CARD NR N01362, FOUND CORROSION ON FLOORBEAM STA 312, RBL 14, WL 208. FLOORBEAM AT BS 312 WAS OUT OF LIMITS. REMOVED DAMAGED BEAM & REPAIRED. INSTALLED NEW SECTION PER SRM 53-10-8 FROM RBL 14 TO LBL 65.
- [SDR 03FDEA01873](https://openairdocs.org/sdr/03FDEA01873.md): Frame · dented · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > FWD LWR CARGO FRAME IS DENTED AT STA 660 STR 22L. FWD LOWER CARGO FRAME IS DENTED AT STR 22L AT BS 660. FOUND TO BE OUT OF LIMITS PER SRM5 3-10-1. REPAIRED DAMAGE FRAME PER SRM 51-40-3.
- [SDR 03FDEA01879](https://openairdocs.org/sdr/03FDEA01879.md): Skin · cracked · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE UPPER LOBE, BS 720B 15.5, STR 15R, CRACKED BS 720B 15.5, STR 16 R/H CRACK FOUND TO BE OUT OF LIMITS. REPAIR DAMAGE STR. 15 RT PER SRM 53-10-3.
- [SDR 03FDEA01870](https://openairdocs.org/sdr/03FDEA01870.md): Shear Tie · corroded · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Structure
  > CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE ON AFT SIDE OF BS 700 FRAME RBL 9 WL 148. REPAIR PER SRM 53-10-4 FIG 13 SHT 1 AT BS 700, RBL 9, WL 148.
- [SDR 03FDEA01880](https://openairdocs.org/sdr/03FDEA01880.md): Frame · corroded · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION FOUND ON FORWARD SIDE OF 970 FRAME AT STR 29 LT. OPEN
- [SDR 03FDEA01878](https://openairdocs.org/sdr/03FDEA01878.md): Skin · bulged · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > N00148 OUTER EXTERIOR SKIN HAS BULGE AT STA 1050 STR 28L ** SD ** COMING
- [SDR 03FDEA01877](https://openairdocs.org/sdr/03FDEA01877.md): Frame · dented · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > N00509) DENT IN FRAME BS 1050 ABOVE STR 25L ** SD ** COMING
- [SDR 03FDEA01875](https://openairdocs.org/sdr/03FDEA01875.md): Floorbeam · corroded · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > N01453 CORROSION WHILE WORKING N01449 FOUND CORROSION ON TOP SURFACE OF UPPER CHORD OF FLOORBEAM BS 1070, RBL 23, WL 208 ** SD ** COMING
- [SDR 03FDEA01874](https://openairdocs.org/sdr/03FDEA01874.md): Frame · dented · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > N00817) FWD LWR CARGO FRAME DENTED AT STA 520 STR 22L TO 25L ** SD ** COMING
- [SDR 03FDEA01872](https://openairdocs.org/sdr/03FDEA01872.md): Floorbeam · corroded · Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > N01482 CORROSION WHILE WORKING CARD NO N00939, FOUND CORROSION ON FLOORBEAM, STA 344 RBL 13-53 WL 208. ** SD ** COMING
- [SDR 03FDEA01863](https://openairdocs.org/sdr/03FDEA01863.md): Stringer · cracked · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > FUSELAGE UPPER LOBE, BS 720B 4.5, STR 15R, CRACKED. REMOVED DAMAGED SECTION OF STRINGER 15R, BS 720B 4.5 AND REPAIRED STRINGER PER SRM 53-10-3 FIG 5.
- [SDR 03FDEA01865](https://openairdocs.org/sdr/03FDEA01865.md): Stringer Clip · cracked · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP BS 950C STR 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 950C, STRINGER 5R PER SRM 51-30-2. LOCATED AND DRILLED HOLES PER SRM 51-30-5.
- [SDR 03FDEA01859](https://openairdocs.org/sdr/03FDEA01859.md): Keelbeam · corroded · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Keel
  > CORROSION ON LOWER CROSS BRACE INSIDE DELTA KEELBEAM, BS 762, WL 148. REMOVED CORROSION ON LOWER CROSS BRACE INSIDE DELTA KEELBEAM BS 762, WL 148. FABRICATED NEW L-ANGLE AND REPLACED CORRODED PART WITH NEW PART PER 727 SRM 53-30-2, 51-40-2, 51-10-2, 51-
- [SDR 03FDEA01857](https://openairdocs.org/sdr/03FDEA01857.md): Frame · dented · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > FWD LWR CARGO FRAME IS DENTED AT STA 560 STR 24 LT. REMOVED DAMAGE AREA AT FRAME IN AREA 1 X 2, AT BS 560, STR 24 LT. FABRICATE THE DOUBLER MADE FROM 7075-T6 0.063, AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.
- [SDR 03FDEA01858](https://openairdocs.org/sdr/03FDEA01858.md): Frame · dented · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Frame
  > FORWARD LOWER CARGO FRAME IS DENTED AT STA 580 STR 24L. REMOVED DAMAGE AT FRAME IN AREA OF 1 X 3 INCHES AT BS 580, STR 24L. FABRICATE THE DOUBLER MADE FROM 7075-T6 0.063 AND INSTALLED THE REPAIR DOUBLER IAW SRM 51-40-3.
- [SDR 03FDEA01860](https://openairdocs.org/sdr/03FDEA01860.md): Shear Tie · corroded · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Structure
  > CORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT SHEAR TIE ON AT SIDE OF BS 700 FRAME LBL 9 WL 148.
- [SDR 03FDEA01861](https://openairdocs.org/sdr/03FDEA01861.md): Floorbeam · corroded · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION AROUND SEVERAL NUT PLATE HOLES IN LONGITUDINAL FLOORBEAM, LBL 25, WL 208, BS 760 - 850.
- [SDR 03FDEA01862](https://openairdocs.org/sdr/03FDEA01862.md): Floorbeam · corroded · Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION BS 400 FLOORBEAM TOP CHORD CORRODED, LBL 6 TO LBL 10, WL 208.

Next page: https://openairdocs.org/deregistered/N270FE-2008-12-17/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 = 'N270FE' AND deregistration_id = 'N270FE-2008-12-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N270FE-2008-12-17/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.