# Service difficulty reports: N274FE, cancelled Aug 27, 2013

A list on [N274FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N274FE-2013-08-27.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 · 58 reports

- [SDR FDEA200905191744](https://openairdocs.org/sdr/FDEA200905191744.md): Wire · damaged · May 19, 2009 · N274FE · Boeing 727233 · Door System Wiring
  > AFTER TAKEOFF AND GEAR RAISED. "MAIN CARGO DOOR B" LIGHT ILLUMINATED. FOLLOWED QRH. DOOR LIGHT EXTINGUISHED RETURNED TO IND. DOOR LIGHT REILLUMINATED ON SHORT FINAL FOR 10 SECONDS. DURING T/S FOUND PIN B PUSHED BACK AT SW S9056 C/P D9834J. THIS IS THE GROUN
- [SDR FDEA200902180572](https://openairdocs.org/sdr/FDEA200902180572.md): Plate · damaged · Feb 18, 2009 · N274FE · Boeing 727233 · Trailing Edge Flap Control System
  > ON CLIMB-OUT ACFT UNUSUAL VIBRATION PASSING 11,000 FT & ACCELERATING THROUGH 335 KIAS. DECREASED AIRSPEED & VIBE STOPPED AT 315 KIAS. ACCELERATED AGAIN & AT FL 180, 325 KIAS VIBE RETURNED, DEPLOYED SPOILERS & VIBE SMOOTHED OUT. STOWED SPOILERS & VIBE RETURN
- [SDR 08FDEA02258](https://openairdocs.org/sdr/08FDEA02258.md): Actuator · out of adjust · Jun 13, 2008 · N274FE · Boeing 727233 · Landing Gear Actuator
  > TEST FLIGHT, RMG SHOWED UNSAFE IND ON THIRD EXTENSION. NO GREEN DOWN AND LOCKED LIGHT, RED DOOR OPEN LIGHT ON. VISUAL INSPECTION BY TOWER AND OTHER A/C CONFIRMED RIGHT MAIN GEAR WAS STILL UP. CYCLED IAW RED TABS AND GOT SAFE DOWN AND LOCKED INDICATION. ADJ
- [SDR 08FDEA02134](https://openairdocs.org/sdr/08FDEA02134.md): Angle · cracked · Jun 3, 2008 · N274FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING INBOARD MID FLAP LOWER AFT CHORD ANGLE IS CRACKED AT WBL 110. CUT OUT DAMAGED SECTION DIM 47 1/4 INCH IAW B727 SRM 51-10-1, FABRICATED FILLER REPAIR USING BAC1503-100046 7075-T6 PO NR 8177105 DIM 47 1/4 INCH BY 2 INCH AND SPLICE USING BAC1503-100046 7
- [SDR 08FDEA01981](https://openairdocs.org/sdr/08FDEA01981.md): Shear Tie · damaged · May 24, 2008 · N274FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT FRAME STA 640 SHEAR TIE LOWER FLANGE HAS A HOLE DRILLED THRU ABOVE STR 27L. FABRICATED 2 EACH FREEZE PLUGS, 2 RETAINING PLATES. INSTALLED FREEZE PLUGS AND RETAINING PLATES IAW EA 7-5310-116985, SRM 51-30-2 AND 51-10-7.
- [SDR 08FDEA01952](https://openairdocs.org/sdr/08FDEA01952.md): Skin · dented · May 22, 2008 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE DENTED BS 297.5 BELOW STR 20R, BELOW FWD LAV SERVICE PANEL CUTOUT FWD LWR CORNER. REWORKED DENT IAW B727 SRM 51-40-1 AND EA 7-5330-116984 AND B727 SRM 53-30-01. REMOVED AND REPLACED RIVET IAW B727 SRM 51-30-. TREATED AND PRIMED AREA IAW B727
- [SDR 08FDEA01938](https://openairdocs.org/sdr/08FDEA01938.md): Stringer · damaged · May 21, 2008 · N274FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT STR 28R LEVELING COMPOUND IS CRACKED AND BULGING AT SPLICE STA 680 PLUS 10 INCHES CUT OUT DAMAGED AREA APPROX DIM 6 3/8 INCH LENGTH, FABRICATED REPAIR SPLICE FROM BAC1498-132 PO NR 8177148 DIM 19 1/2 INCH LENGTH AND FILLER FROM BAC1498-143 PO N
- [SDR 08FDEA01862](https://openairdocs.org/sdr/08FDEA01862.md): Skin · damaged · May 16, 2008 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > SKIN OIL CANNED LEFT FUSELAGE STA 1243 STR 18L TO 19L. CUT OUT DAMAGED AREA APPROX DIM 3 7/8 BY 1 7/8, FABBED REPAIR DOUBLER FROM 2024- T3.063 PO NR 9006713 APPROX DIM 13 3/4 BY 8 1/2 AND INSTALLED REPAIR DOUBLER AT BS 1243 STR 18-19 LEFT IAW B727 SRM 53-30
- [SDR 08FDEA01861](https://openairdocs.org/sdr/08FDEA01861.md): Skin · damaged · May 16, 2008 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > STA 660 AT PREVIOUS REPAIR STR 28L TO 28R EXTERIOR SKIN BULGED AND CRACKED NEAR L/E OF REPAIR, BULGING NEAR T/E. MANY FASTENERS SHOW EVIDENCE OF WORKING AND CORROSION. REMOVED PREVIOUS DOUBLER IAW B727 SRM 51-30-2, CUTOUT DAMAGED AREA DIM 17 INCH BY 11 INCH
- [SDR 08FDEA01859](https://openairdocs.org/sdr/08FDEA01859.md): Skin · damaged · May 16, 2008 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > SKIN BULGE LT FUSELAGE STA 1323 ABOVE STRL 18. CUTOUT DAMAGED AREA APPROX 2 7/8 INCH BY 2 INCH IAW B727 SRM 53-30-3 FIG 14, FABRICATED DOUBLER REPAIR MATERIAL 2024-T3.063 PO NR 9006773 DIM 11 INCH BY 10 INCH FILLER MATERIAL 2024-T3.050 PO NR 9006742 DIM 2 I
- [SDR 08FDEA01863](https://openairdocs.org/sdr/08FDEA01863.md): Skin · dented · May 16, 2008 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DENT RT FUSELAGE STA 540 STR 24R (RVSM AREA). REPAIRED DENT IAW EA 7-5330-116983.
- [SDR 08FDEA01860](https://openairdocs.org/sdr/08FDEA01860.md): Skin · misrepaired · May 16, 2008 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXISTING DOUBLER REPAIR TO THE FUSELAGE SKIN AT BS 1140 AND STR 20L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, FABRICATED NEW DOUBLER. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 3 AND SRM 53-30-3 FIG 14 AND SRM 51-3
- [SDR 08FDEA01858](https://openairdocs.org/sdr/08FDEA01858.md): Support · corroded · May 16, 2008 · N274FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AT BS 1105 UNDER STR 29R SHOWS CORROSION. FABRICATED NEW SUPPORT CHANNEL FOR STR 29R BS 1105 AND INSTALLED NEW CHANNEL IAW SRM 51-10-3, SRM 51-20- 01 FIG 3 AND DWG NR 65-56136, FABRICATED REPAIR DOUBLER, INSTALLED SHEAR TIE REPAIRS IAW
- [SDR 08FDEA01051](https://openairdocs.org/sdr/08FDEA01051.md): Actuator · failed · Mar 19, 2008 · N274FE · Boeing 727233 · Landing Gear Door Actuator
  > RED GEAR DOORS LIGHT AND RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AMBER RIGHT GEAR DOOR LIGHT ON S/O PANEL ALSO ILLUMINATED. REPLACED RT MAIN GEAR ACTUATOR IAW AMM 32-32-002-4, AND RT MAIN GEAR CYCLES UP AND DOWN NORMAL WITH NO LEAKS NO
- [SDR 08FDEA00510](https://openairdocs.org/sdr/08FDEA00510.md): Control Valve · failed · Feb 19, 2008 · N274FE · Boeing 727233 · Air Intake Anti/De-Ice System
  > AT ROTATION NR 2 DUCT ANTI-ICE OVERHEAT LIGHT ILLUMINATED TEMP OFF SCALE HIGH. AN QRH FOR ANTI-ICE DUCT OVERHEAT LIGHT. NR 2 ENGINE COULD NOT BE OPERATED ABOVE 1.25 EPR NR 2 DUCT OVERHEAT LIGHT ON MEL 30-11-A NR 2 ENGINE 13TH STAGE VALVE OPEN GOC ADVISED AIR
- [SDR 07FDEA02378](https://openairdocs.org/sdr/07FDEA02378.md): None · unknown · Jul 5, 2007 · N274FE · Boeing 727233 · Landing Gear Position and Warning
  > ON TAKEOFF, RT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH, RECYCLED GEAR AND LIGHT EXTINGUISHED. CONTINUED FLIGHT. INSPECTED GEAR DOOR SWITCHES CK GOOD, CYCLE DOOR OPEN CLOSED SEVERAL TIME. OPS CHECKS NORMAL IAW AMM 32-62-011-5.
- [SDR 07FDEA01003](https://openairdocs.org/sdr/07FDEA01003.md): Actuator · leaking · Mar 18, 2007 · N274FE · Boeing 727233 · Leading Edge Slat Actuator
  > SHORT FINAL, LOSS OF A SYSTEM, LANDED STRAIGHT AHEAD. TOWED IN. AFTER T/S FOUND NR 2 L/E FLAP ACTUATOR LEAKING. CANCELED FIRST PART. REMOVED AND REPLACED NR 2 LE FLAP ACT IAW M/M 27-81-022-4. SERVICED HYD SYSTEM PER 12-12-000-2.
- [SDR 06FDEA1728](https://openairdocs.org/sdr/06FDEA1728.md): Engine · seized · May 6, 2006 · N274FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > AFTER T/O AT 1,000' WITH STD POWER, NR 3 ENGINE SEIZED AT QUIET OIL QUANTITY DROPPED TO ZERO. CONDUCTED EPR REDUCTION. QRH ENGINE FIRE/SEVERE DAMAGE CHECKLIST. RETURNED TO FIELD. CRASH CREW REPORTED OIL LEAKING FROM ENGINE. PERFORMED ENGINE SEIZURE INSP P
- [SDR 05FDEA04423](https://openairdocs.org/sdr/05FDEA04423.md): Skin · gouged · Dec 29, 2005 · N274FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > A GOUGE FOUND AT BS 950E, STR 19R DURING PRIMARY INSPECTION, REPAIR ACCOMPLISHED WITH EA 7-5330-92374 ISSUED BY FEDEX ENGINEERING, REPAIR IS CLASSIFIED AS MAJOR PER EA 7-5330-92374.
- [SDR 05FDEA04389](https://openairdocs.org/sdr/05FDEA04389.md): Repair · unknown · Dec 21, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1140, STR 20L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP OF THE INSTALLA
- [SDR 05FDEA04381](https://openairdocs.org/sdr/05FDEA04381.md): Repair · misinstalled · Dec 20, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FOUND PREVIOUSLY REPAIR AT STA 1183, STR 27R IS NOT IN CONFORMANCE WITH APPROVED FAA DATA. REMOVED EXISTING REPAIR, ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
- [SDR 05FDEA04380](https://openairdocs.org/sdr/05FDEA04380.md): Repair · misinstalled · Dec 20, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FOUND PREVIOUSLY REPAIR AT STA 1140, STR 22L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 1, TABLE 1, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
- [SDR 05FDEA04376](https://openairdocs.org/sdr/05FDEA04376.md): Repair · undamaged · Dec 19, 2005 · N274FE · Boeing 727233 · Elevator Structure
  > FOUND PREVIOUSLY INSTALLED REPAIR ON UPPER SURFACE OF LT ELEVATOR WAS ACCOMPLISHED IAW ENGINEERING REPAIR NR 16-0193, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL
- [SDR 05FDEA04375](https://openairdocs.org/sdr/05FDEA04375.md): Repair · undamaged · Dec 19, 2005 · N274FE · Boeing 727233 · Aircraft Structures
  > FOUND PREVIOUSLY INSTALLED REINFORCEMENT DOUBLER AT STA 344 BETWEEN STR 4L AND 5L WAS ACCOMPLISHED IAW RIGID BARRIER MODIFICATION DOCUMENT EA 7-5340-7-5002, PAGE 1 AND VENTURA AEROSPACE DWG 2942, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, S
- [SDR 05FDEA04374](https://openairdocs.org/sdr/05FDEA04374.md): Repair · undamaged · Dec 19, 2005 · N274FE · Boeing 727233 · Aircraft Structures
  > FOUND PREVIOUSLY INSTALLED REPAIR AT STA 720D, STR 19R WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR
- [SDR 05FDEA04373](https://openairdocs.org/sdr/05FDEA04373.md): Repair · undamaged · Dec 19, 2005 · N274FE · Boeing 727233 · Aircraft Structures
  > FOUND PREVIOUSLY INSTALLED REPAIR AT AFT LOWER CORNER OF FWD GALLEY DOOR CUT OUT WAS ACCOMPLISHED IAW SB 727-53-0188, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL
- [SDR 05FDEA04372](https://openairdocs.org/sdr/05FDEA04372.md): Repair · undamaged · Dec 19, 2005 · N274FE · Boeing 727233 · Aircraft Structures
  > FOUND PREVIOUSLY INSTALLED REPAIR AT STA 680, STR 28 WAS ACCOMPLISHED IAW SRM 51-40-3, FIG 1 PAGE 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REP
- [SDR 05FDEA04371](https://openairdocs.org/sdr/05FDEA04371.md): Repair · none · Dec 19, 2005 · N274FE · Boeing 727233 · Aircraft Structures
  > FOUND PREVIOUSLY INSTALLED REPAIR AT LT ENTRY DOOR STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT.2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, R
- [SDR 05FDEA04370](https://openairdocs.org/sdr/05FDEA04370.md): None · none · Dec 19, 2005 · N274FE · Boeing 727233 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 28R TO 28L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 2, PAGE 9, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMAN
- [SDR 05FDEA04344](https://openairdocs.org/sdr/05FDEA04344.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Wing Structure
  > FOUND PREVIOUS REPAIR ON UPPER LEADING EDGE OF LEFT WING AT NR 3 LEADING EDGE SLAT WAS ACCOMPLISHED IAW SRM 57-30-4, FIG 1. BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL
- [SDR 05FDEA04343](https://openairdocs.org/sdr/05FDEA04343.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727233 · Wing Structure
  > FOUND PREVIOUSLY REPAIR ON LT INBOARD FORE FLAP LEADING EDGE WAS ACCOMPLISHED IAS SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS
- [SDR 05FDEA04342](https://openairdocs.org/sdr/05FDEA04342.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727233 · Wing Structure
  > FOUND PREVIOUS REPAIR ON LT OUTBOARD FOREFLAP LEADING EDGE WAS ACCOMPLISHED IAW SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING AND GENERAL WORKMANSHIP, REPAIR
- [SDR 05FDEA04341](https://openairdocs.org/sdr/05FDEA04341.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Wing Structure
  > FOUND PREVIOUS REPAIR ON LOWER SURFACE OF RIGHT INBOARD AFT FLAP WAS ACCOMPLISHED IAW SRM 57-50-4 FIG 5, PAGE 12, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPA
- [SDR 05FDEA04340](https://openairdocs.org/sdr/05FDEA04340.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Wing Structure
  > FOUND PREVIOUS REPAIR ON RIGHT WING NR 7 L/E SLAT WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 1 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PE
- [SDR 05FDEA04339](https://openairdocs.org/sdr/05FDEA04339.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Wing Structure
  > FOUND PREVIOUS REPAIR ON LEFT WING NR 1 KRUEGER FLAP FWD SURFACE WAS ACCOMPLISHED IAW SRM 57-50-3, FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASS
- [SDR 05FDEA04337](https://openairdocs.org/sdr/05FDEA04337.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Wing Structure
  > FOUND PREVIOUSLY REPAIR AT NR 5 KRUEGER FLAP WS 265.0 WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3, BASED ON EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, NUMBER OF FASTENERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS
- [SDR 05FDEA04336](https://openairdocs.org/sdr/05FDEA04336.md): None · none · Dec 15, 2005 · N274FE · Boeing 727200 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR AT RT WING NR 6 KRUEGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, NUMBERS OF FASTENER AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED
- [SDR 05FDEA04335](https://openairdocs.org/sdr/05FDEA04335.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Fuselage Main, Structure
  > FOUND PREVIOUSLY REPAIR AT STA 950A, STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 3 PAGE 13, BASED ON EXTERNAL VISUAL EVALUATION OF LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED
- [SDR 05FDEA04333](https://openairdocs.org/sdr/05FDEA04333.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Fuselage Main, Structure
  > FOUND REPAIR AT STA 950A, STR 29R WAS DETERMINED HAD BEEN ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS, MATERIAL THICKNESS AND TYPE AND GENERAL WORKMANS
- [SDR 05FDEA04331](https://openairdocs.org/sdr/05FDEA04331.md): Repair · unknown · Dec 15, 2005 · N274FE · Boeing 727200 · Wing Main, Frame Structure
  > FOUND REPAIR LOCATED ON RIGHT WING L/E WING ROOT REPAIR REQUIRES EVALUATION FOR COMPLIANCE WITH FAA APPROVED DATA. REPAIR WAS DETERMINED ACCOMPLISHED IAW SRM 57-30-4 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED OF LOCATION, SH
- [SDR 02FDEA00136](https://openairdocs.org/sdr/02FDEA00136.md): Switch · faulty · Feb 20, 2002 · N274FE · Boeing 727233 · Trailing Edge Flap Control System
  > 02-51 ON RETRACT OF FLAPS AMBER LED LIGHT ON. R&R #1 L/E FLAPS POSITION SWITCH PER IAW MM 27-82-001-4. OPS CHECK GOOD.
- [SDR 00FDEA00866](https://openairdocs.org/sdr/00FDEA00866.md): Floorbeam · damaged · Dec 8, 2000 · N274FE · Boeing 727233 · Fuselage Main, Floor Beam
  > NR 911 DOUBLE FASTENER HOLES IN FLOORBEAM AT BS 380, LBL 13, WL 208. ** S/D ** R&R PER FEDEX SRM 53-10-8, FIG 8.
- [SDR 00FDEA00857](https://openairdocs.org/sdr/00FDEA00857.md): Frame · dented · Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Frame
  > NR 339- DENTED FRAME BS 660, 2 INCHES ABOVE STRINGER 26R. ** S/D ** R&R PER FEDEX SRM 51-40-3.
- [SDR 00FDEA00856](https://openairdocs.org/sdr/00FDEA00856.md): Frame · dented · Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Frame
  > NR 333, DENTED FRAME BS 600, 2 INCHES ABOVE STR 26L. ** S/D ** R&R PER FEDEX SRM 51-40-3, 51-30-2.
- [SDR 00FDEA00855](https://openairdocs.org/sdr/00FDEA00855.md): Frame · dented · Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Frame
  > NR 332 DENTED FRAME BS 580, 2 INCHES ABOVE STRINGER 26L. ** S/D ** R&R PER FEDEX SRM 51-40-3, 51-30-2.
- [SDR 00FDEA00854](https://openairdocs.org/sdr/00FDEA00854.md): Frame · corroded · Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Frame
  > NR 836 CORROSION (C53-224-01(2)) ON SEVERAL NUTPLATES AND FASTENER HOLES ON LONGITUDINAL BEAM FROM BS 740 TO 850, LBL 45, WL 208. ** S/D ** R&R PER DWG 65-16279, FEDEX SRM 51-30-2.
- [SDR 00FDEA00853](https://openairdocs.org/sdr/00FDEA00853.md): Floorbeam · damaged · Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Floor Beam
  > NR 907 MECHANICAL DAMAGE ON FLOORBEAM BS 312, LBL 3, WL 208. ** S/D ** R&R PER FEDEX EA 7-5310-53867.
- [SDR 00FDEA00852](https://openairdocs.org/sdr/00FDEA00852.md): Stringer · corroded · Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > NR 340 CORROSION (C53-111-01(2)) AT STRINGER 28L SPLICE BS 685-675. ** S/D ** R&R & FAB PER FEDEX SRM 51-10-6, 51-30-2
- [SDR 00FDEA00842](https://openairdocs.org/sdr/00FDEA00842.md): Floorbeam · corroded · Nov 30, 2000 · N274FE · Boeing 727233 · Fuselage Main, Floor Beam
  > NR 862 (C53-224-01) CORROSION ON FLOORBEAM BS 620, LBL 25, TO LBL 44.5, WL 208. ** S/D ** R&R PER FEDEX SRM 53-10-8 FIG 8.
- [SDR 00FDEA00837](https://openairdocs.org/sdr/00FDEA00837.md): Keelbeam · corroded · Nov 30, 2000 · N274FE · Boeing 727233 · Fuselage Main, Keel
  > NR 303 CORROSION ON KEELBEAM BS 780, LBL 5, WL 148. ** S/D ** R&R PER FEDEX EA 7-5310-53871.

Next page: https://openairdocs.org/deregistered/N274FE-2013-08-27/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 = 'N274FE' AND deregistration_id = 'N274FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N274FE-2013-08-27/reports

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