# Service difficulty reports: N283FE, cancelled Aug 27, 2013

A list on [N283FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N283FE-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.

- [SDR FDEA201010063955](https://openairdocs.org/sdr/FDEA201010063955.md): Duct · failed · Oct 6, 2010 · N283FE · Boeing 727233 · Engine Bleed Air System
  > ENGINE FAIL LIGHT ILLUMINATED AT 100 KTS ON T/O OAT 10. 169,000 TOGW. REJECTED T/O CHECKLIST COMPLIED WITH. R & R NR 2 ENGINE N1 GAUGE AS PRECAUTIONARY IAW AMM 31-00-011-4. RAN NR 2 ENGINE IAW JRH CHAPTER 6, ALL ENGINE PARAMETERS WERE NORMAL. ON RETURN TO
- [SDR FDEA201005281704](https://openairdocs.org/sdr/FDEA201005281704.md): Connector · defective · May 28, 2010 · N283FE · Boeing 727233 · Flight Control System Wiring
  > CREW PERFORMED AN AIR TURN BACK TO MEM FOR AN UNSAFE INDICATION ON THE NR 3 L/E SLAT. WHEN CREW WENT FROM FLAPS 5 TO 2 THEY HAD AN UNSAFE INDICATION ON NR 3 L/E SLAT. WHEN CREW RETURNED TO FLAPS 5 THE UNSAFE INDICATION WENT AWAY. NR 3 LED UNSAFE WHEN RAISIN
- [SDR FDEA200904041180](https://openairdocs.org/sdr/FDEA200904041180.md): Skin · gouged · Apr 4, 2009 · N283FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA STA 660 S2L GOUGE ON SKIN NEXT TO UPPER INTERCOSTAL EXTENSION. REPAIRED GOUGE ON INNER SKIN AT STA 660 STR 2L IAW FX P - F SRM STC SA1767SO AND SA1768SO FIG 1B SRM 53-30-3. BLENDED GOUGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1. CUT OU
- [SDR FDEA200904021163](https://openairdocs.org/sdr/FDEA200904021163.md): Skin · cracked · Apr 2, 2009 · N283FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LT AFT SERVICE DOOR (L-2) FWD LOWER SIDE SKIN HINGE CUT-OUT AT UPPER AFT CORNER HAS ABOUT 1/2 INCH LONG CRACK AT SKIN RADIUS. TRIMMED OUT CRACK AREA IAW FX EA 7-5210-126807 ITEM 1. NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. FABRICATED FILLER AND REPAIR ANGL
- [SDR FDEA200904021162](https://openairdocs.org/sdr/FDEA200904021162.md): Skin · cracked · Apr 2, 2009 · N283FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LT AFT SERVICE DOOR (L-2) FWD UPPER SIDE SKIN HINGE CUT-OUT AT LWR AFT CORNER HAS ABOUT 1 INCH LONG CRACK AT SKIN RADIUS. TRIMMED OUT CRACK AREA IAW EA 7-5210-126807 ITEM 1. HFEC INSPECTED AREA IAW NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. FABRICATED FILL
- [SDR FDEA200903261076](https://openairdocs.org/sdr/FDEA200903261076.md): Web · cracked · Mar 26, 2009 · N283FE · Boeing 727233 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 NOSE COWL INTERIOR WEB IS CRACKED, 2 PLACES AT LIGHTNING HOLE, NAC STA 77.5 REMOVED AFT LOWER PANEL AT NR 1 ENG NOSE COWL FOR FOM IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. HFEC INSPECTION PERFORMED IAW NDTM 51-00-00 FIG 23, PT 6. NO DEFECT
- [SDR 08FDEA02169](https://openairdocs.org/sdr/08FDEA02169.md): Hydraulic System · malfunctioned · Jun 5, 2008 · N283FE · Boeing 727233 · Hydraulic System, Main
  > DURING DESCENT LOST ALL OF SYS A HYD QUANITY PRESSURE WAS NORMAL - 3000 PSI AND NO A.R.E. OR ENG PUMP LOW PRESSURE LIGHTS WERE ILLUMINATED AFTER TEN MINUTES BOTH ENG 1 AND ENG 2 LOW PRESSURE LIGHTS STARTED TO FLASH. TURNED BOTH SYSTEM OFF AT THE PUMP SWITC
- [SDR 08FDEA00663](https://openairdocs.org/sdr/08FDEA00663.md): Hose · chafed · Feb 29, 2008 · N283FE · Boeing 727233 · Hydraulic System, Main
  > IN FLIGHT TOTAL LOSS OF "A" SYSTEM HYDRAULICS. "A" SYSTEM HYD QTY WAS FOUND AT 2 GALLON SYSTEM DID NOT RUN EMPTY. FOUND HYD LINE IN ELEVATOR PCP BROKEN AT CLAMPED AREA. REPLACED LINE REF MM 20-10-012-4. OPERATED HYD SYSTEM. OPERATED AND INSPECTED ALL FL
- [SDR 07FDEA04523](https://openairdocs.org/sdr/07FDEA04523.md): Frame · cracked · Sep 30, 2007 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > FWD LOWER CARGO STUB FRAME AT STA 580 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 STUB FRAME, FABRICATED AND INSTALLED NEW STUB FRAME IAW 727 SRM 51-10-01 AND DWG 53FX1370.
- [SDR 07FDEA04522](https://openairdocs.org/sdr/07FDEA04522.md): Frame · cracked · Sep 30, 2007 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > FWD CARGO, LOWER STUB FRAME EXTENSION AT STA 600 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 STUB FRAME, FAB'D AND INSTALLED A NEW STUB FRAME IAW SRM 51-10-01 AND DWG 53FX1370.
- [SDR 07FDEA01223](https://openairdocs.org/sdr/07FDEA01223.md): Relay · failed · Mar 31, 2007 · N283FE · Boeing 727233 · Smoke Detection
  > FIRE WARNING MASTER LIGHTS ILLUMINATED, INTERMITTENTLY, WITH AUDIO BELL. NO OTHER INDICATIONS. REMOVED AND REPLACED R97 RELAY AND M438, REF WIRING DIAGRAM MANUAL 49-41-01 PAGE 3. NEEDS OPS CHECKS. REF MM 26-15-000, OP CHECK APE FIRE SYSTEM. CHECKS OK.
- [SDR 06FDEA03468](https://openairdocs.org/sdr/06FDEA03468.md): Web · corroded · Sep 28, 2006 · N283FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT BILGE AREA SUPPORT WEB HAS CORROSION BETWEEN STA 1070-1090 RBL 3. FABRICATED NEW WEB ON TRVLR T6/629725. LOCATED AND DRILLED NEW WEB IAW SRM 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW WEB IAW 51-30-2 SRM.
- [SDR 04FDEA01056](https://openairdocs.org/sdr/04FDEA01056.md): Skin · dented · Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5.
- [SDR 04FDEA01055](https://openairdocs.org/sdr/04FDEA01055.md): Frame · gouged · Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Frame
  > FRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO.023 INCH DEEP. FRAME THICKNESS IS.050 OUT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. INSTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51-30-5.
- [SDR 04FDEA01054](https://openairdocs.org/sdr/04FDEA01054.md): Skin · dented · Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3.
- [SDR 04FDEA001056](https://openairdocs.org/sdr/04FDEA001056.md): Skin · dented · Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5.
- [SDR 04FDEA001055](https://openairdocs.org/sdr/04FDEA001055.md): Frame · gouged · Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Frame
  > FRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO.023 INCHES DEEP. FRAME THICKNESS IS.050 OUT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. ISNTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51-30-5.
- [SDR 04FDEA001054](https://openairdocs.org/sdr/04FDEA001054.md): Skin · dented · Apr 22, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3.
- [SDR 04FDEA00981](https://openairdocs.org/sdr/04FDEA00981.md): Skin · bulged · Apr 16, 2004 · N283FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE SKIN BULGE AT BS 380 BETWEEN STR 17L AND STR 18L. FOUND BULGE IN SKIN, BS 380 BETWEEN STR 17L & 18L, TO BE CREASED AND OUT OF LIMITS IAW SRM 53-30-1.CUT OUT DAMAGED SKIN 2 X 6 AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3.
- [SDR 04FDEA00980](https://openairdocs.org/sdr/04FDEA00980.md): Web · cracked · Apr 16, 2004 · N283FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > SHEAR WEB CRACKED, AT BS 380-400, LBL 65, WL 208. REMOVED CRACKED SHEAR WEB BS 380-400, LBL 65, WL 208. FABRICATED NEW WEB AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND FED EX MM 51-20-151.
- [SDR 04FDEA00979](https://openairdocs.org/sdr/04FDEA00979.md): Stringer · cracked · Apr 16, 2004 · N283FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > STR 17L IS CRACKED AT BS 385 LBL 65 WL 208. CUT AND REMOVED STR AND INSTALLED REPAIR AT BS 370 TO BS 407, STR 17L, WL 208 IAW SRM 51-40-4.
- [SDR 04FDEA00147](https://openairdocs.org/sdr/04FDEA00147.md): Powerpack · contaminated · Jan 13, 2004 · N283FE · Boeing 727200 · Stabilizer Control System
  > WITH AUTOPILOT DISENGAGED AT CRUISE FLT, UNCOMMANDED FWD/AFT MOVEMENT OF CONTROL WHEEL HAD TO BE COUNTER-ACTED WITH FIRM PRESSURE. UNCOMMANED MOVEMENT OF CONTROL WHEEL SEEMED TO LESSEN WITH SLOWER AIRSPEED (310-200 KIAS). THIS PROBLEM WAS DISCOVERED AFTER DI
- [SDR 03FDEA01096](https://openairdocs.org/sdr/03FDEA01096.md): Structure · noisy · Jul 13, 2003 · N283FE · Boeing 727200 · Aircraft Structures
  > PASSING 10K MSL, EXTREMELY LOUD SQUEAL APPEARED IN COCKPIT. PRESSURIZATION NORMAL. CLIMBED TO 14K AND SQUEAL REMAINED ON. NOISE WENT OUT PASSING 10K MSL IN DESCENT. SHUT OFF ALL RADIOS & COULD NOT ISOLATE PROBLEM. PRESSURIZED A/C TO 8.5 PSI NO SQUEAL OR H
- [SDR 02FDEA00248](https://openairdocs.org/sdr/02FDEA00248.md): Accessory Unit · failed · Apr 16, 2002 · N283FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > 02-92 LAND GEAR W/N RETRACT AFTER TAKEOFF, LG LATCH CIRCUIT BREAKER POPPED AND WOULD NOT RESET. R&R LG ACCESSORY UNIT PER MM 32-09-121. OPS CK NORM.
- [SDR 02FDEA00245](https://openairdocs.org/sdr/02FDEA00245.md): Smoke Detector · faulty · Apr 11, 2002 · N283FE · Boeing 727233 · Smoke Detection
  > ON CLIMB LWR FWD CARGO SMOKE WARNING LIGHT AND BELL CAME ON. REMOVED AND REPLACED NR 1 & 2 FWD LWR CARGO COMP FIRE SUPPRESSION BOTTLES PER MM 26-17-014-2. INSTALL NEW FIRE EXTINGUISHER. REMOVED AND REPLACED 4 FWD CARGO COMP SMOKE DETECTION UNITS.
- [SDR 02FDEA00227](https://openairdocs.org/sdr/02FDEA00227.md): Fire Warning · false activation · Apr 5, 2002 · N283FE · Boeing 727233 · Fire Detection
  > DURING CLIMBOUT FIRE IND ON APU. APU MASTER SWITCH OFF AND IND SHOW NORMAL SHUTDOWN. REMOVED AND REPLACED APU FIRE AND OVERHEAT DET SYS PER PRECAUTIONARY MM 26-15-003-4.
- [SDR 02FDEA00277](https://openairdocs.org/sdr/02FDEA00277.md): Apu · fire · Apr 5, 2002 · N283FE · Boeing 727233 · Airborne Auxiliary Power Unit (APU) System
  > 02-86 DURING CLIMBOUT, FIRE IN APU. SHUTDOWN APU. REMOVED AND REPLACED APU, FIRE OVERHEAT DETECTOR, FIRE BOTTLE AND SQUIB ASSEMBLY.
- [SDR 01FDEA00022](https://openairdocs.org/sdr/01FDEA00022.md): Wire · failed · Jan 16, 2001 · N283FE · Boeing 727233 · Leading Edge Slat Control System
  > DURING FLAP RETRACT (FROM 5 DEG TO 2 DEG) DID NOT GET A GREEN LEAD EDGE FLAP LIGHT, 2ND OFF. POSITION IND SHOW NR 7 INTRANSIT. *S/D* REPAIRED WIRES AS PER CHAP 20 WIRING DIAGRAM PER 27-81-01, 27-82-00-1.
- [SDR 99FDEA00098](https://openairdocs.org/sdr/99FDEA00098.md): Connector · dirty · Mar 11, 1999 · N283FE · Boeing 727233 · Cabin Pressure Control System
  > 99-0066 - AC WON'T PRESSURIZE. COMP RED TABS AND PULL CIRCUIT BREAKERS ON P2 PNL BUT CABIN OUTFLOW VALVE REMAIN STUCK IN THE FULL OPEN POS. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, NO HELP, CONTROLLER NEED LEAK CK. PERF LOW LEVEL STATIC LEAK CK OF AU
- [SDR 97FDEA00168](https://openairdocs.org/sdr/97FDEA00168.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0181 010, DENTED FRAME AT 680, LBL 40, WL 164. * S/D* REMOVED DAMAGED AREA OF FRAME AT BS 680, LBL 40, WL 164. REPAIRED FRAME PER FED-EX SRM 53-10-1 AND FED-EX SRM 51-40-3 FIG 1.
- [SDR 97FDEA00167](https://openairdocs.org/sdr/97FDEA00167.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0180 119. DENTED FRAME AT BS 600, LBL 31-40, WL 163. *** S/D *** COMING.
- [SDR 97FDEA00166](https://openairdocs.org/sdr/97FDEA00166.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0179 009, DENTED FRAME AT BS 520, LBL 35, WL 163. *S/D* REMOVED DAMAGE 1 BY 2, FABRICATED AND INSTALLED REPAIR DOUBLER PER FED-EX SRM 53-10-2 AND 51-40-3.
- [SDR 97FDEA00165](https://openairdocs.org/sdr/97FDEA00165.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0178 011, DENTED FRAME AT BS 500, LBL 28 TO 35, WL 161. *S/D* REPAIRED FRAME BS 500, LBL 28 TO 35 PER FED-EX SRM 51-40-3 FIG 1.
- [SDR 97FDEA00164](https://openairdocs.org/sdr/97FDEA00164.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0177 012, DENTED FRAME AT BS 560, LBL 39, WL 164. *S/D* FABRICATED AND INSTALLED REPAIR PER FED-EX SRM 51-40-3, 53-10-1 AND 53-10-2.
- [SDR 97FDEA00163](https://openairdocs.org/sdr/97FDEA00163.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0175 013, DENTED FRAME AT BS 500, RBL 41, WL 164. *S/D* REMOVED DAMAGED AREA AT BS 500, RBL 41, WL 164. FABRICATED REPAIR DOUBLER AND INSTALLED PER FED-EX SRM 51-40-3 FIG 1.
- [SDR 97FDEA00162](https://openairdocs.org/sdr/97FDEA00162.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0174014 DENTED FRAME AT BS 520, RBL 38, WL 164. REMOVED DAMAGED AREA OF FRAME AT BS 520, RBL 38, WL 164. REPAIRED FRAME PER FED-EX SRM 51-40-3.
- [SDR 97FDEA00161](https://openairdocs.org/sdr/97FDEA00161.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0173015 DENTED FRAME AT BS 660, RBL 32-40,WL 163. REMOVED DAMAGED AREA AT BS 660, RBL 32 - 40, WL 163. FABRICATED PART, ALODINED AND PRIMED REPAIR FOR FRAME CUTOUT AND INSTALLED PER FED-EX SRM 51-40-3 FIG 1.
- [SDR 97FDEA00160](https://openairdocs.org/sdr/97FDEA00160.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0172016 DENTED FRAME AT BS 680, RBL 32-40, WL 163. CUT OUT DENT IN FRAME AT BS 680, RBL 32 - 40, WL 163 AND REPAIRED FRAME PER FED-EX SRM 51-40-3 FIG 1.
- [SDR 97FDEA00159](https://openairdocs.org/sdr/97FDEA00159.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0162 017 FRAME DENTED AT BS 1148, LBL 22. REMOVED 1.25 BY 1 DAMAGE. FABRICATED AND INSTALLED REPAIR PER FED-EX SRM 51-40-3.
- [SDR 97FDEA00158](https://openairdocs.org/sdr/97FDEA00158.md): Frame · dented · Mar 13, 1997 · N283FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0161 018 FRAME DENTED AT BS 970, LBL 28. REPAIRED DAMAGED FRAME BS 970, LBL 28, WL 148 PER FED-EX SRM 51-40-3 FIG 1.
- [SDR 97FDEA00153](https://openairdocs.org/sdr/97FDEA00153.md): Web · corroded · Mar 12, 1997 · N283FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NR 0343 008, CORROSION IN SEVERAL AREAS ON HORIZONTAL WEB JUST BELOW NR 2 WINDOW TRACK BS 227 TO 255, LBL 48 TO 51, WL 228 TO 234. *S/D* REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. CUT OUT DAMAGED AREA AND REPAIRED IAW FED-EX SRM 51
- [SDR 97FDEA00152](https://openairdocs.org/sdr/97FDEA00152.md): Clip · cracked · Mar 11, 1997 · N283FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NR 0170 007, STRINGER CLIPS CRACKED AT BS 580, STR 25, 24 AND 23 L. *S/D* REMOVED, FABRICATED AND INSTALLED NEW STRINGER CLIPS AT BS 580, STRINGERS 23, 24 AND 25L IAW FED-EX SRM 51-10-1, 51-30-2.
- [SDR 97FDEA00146](https://openairdocs.org/sdr/97FDEA00146.md): Flap · delaminated · Mar 10, 1997 · N283FE · Boeing 727233 · Trailing Edge Flaps
  > NR 0139 003. RIGHT WING O/B FORE FLAP HAS TWO AREAS OF DELAMINATION ON O/B UPPER SURFACE. REMOVED DAMAGE AND REPAIRED SKIN TO RIGHT WING O/B FORE FLAP IAW FED-EX SRM 51-40-6.
- [SDR 97FDEA00145](https://openairdocs.org/sdr/97FDEA00145.md): Flap · delaminated · Mar 10, 1997 · N283FE · Boeing 727233 · Trailing Edge Flaps
  > NR 0421 002, LT WING I/B MIDFLAP HAS AREA OF DELAMINATION ON T/E WS 100. *S/D* REPAIRED LT WING I/B MIDFLAP T/E DELAMINATION AT T/E WS 100 IAW FED-EX SRM 51-40-6.
- [SDR 97FDEA00149](https://openairdocs.org/sdr/97FDEA00149.md): Floorbeam · corroded · Mar 9, 1997 · N283FE · Boeing 727233 · Fuselage Main, Floor Beam
  > NR 0482006 CORROSION (C53-224-01) ON 344 FLOORBEAM, LBL 13- RBL 11, WL 207.5. CORROSION FOUND TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REMOVED AND REPLACED 344 FLOORBEAM UPPER CHORD IAW FED-EX SRM 53-10-8.
- [SDR 97FDEA00148](https://openairdocs.org/sdr/97FDEA00148.md): Bonding Strap · corroded · Mar 7, 1997 · N283FE · Boeing 727233 · Leading Edge Devices
  > NR 0259 005. CORROSION (C57-562-01-2) NR 6 K-FLAP TO BULLNOSE JUMPER ATTACH POINT IS CORRODED AT UPPER ATTACH POINT. REMOVED CORROSION ON NR 6 K-FLAP BULL NOSE UPPER BONDING JUMPER ATTACH POINT IAW FED-EX E.A. NR 7-5740-32908.
- [SDR 97FDEA00147](https://openairdocs.org/sdr/97FDEA00147.md): Flap · corroded · Mar 7, 1997 · N283FE · Boeing 727233 · Leading Edge Devices
  > CORROSION (C57-562-01-2) NR 4 K-FLAP TO BULLNOSE BONDING JUMPER ATTACH POINT IS CORRODED AT UPPER ATTACH POINT. REPAIRED NR 4 K-FLAP TO BULL NOSE BONDING JUMPER ATTACHED POINT IAW FED-EX SR DRAWING 27-57-010C AND SRM 57-50-3.
- [SDR 97FDEA00143](https://openairdocs.org/sdr/97FDEA00143.md): Flap · corroded · Mar 7, 1997 · N283FE · Boeing 727233 · Leading Edge Devices
  > NR 260 001 CORROSION (C57-562-01-2) UNDERNEATH NR 6 K-FLAP DATA PLATE. REMOVED CORROSION AND REPAIRED K-FLAP IAW FED-EX SRM 57-30-3.

## 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 = 'N283FE' AND deregistration_id = 'N283FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N283FE-2013-08-27/reports

---
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