# Service difficulty reports: N287FE, cancelled Mar 19, 2013

A list on [N287FE, cancelled Mar 19, 2013](https://openairdocs.org/deregistered/N287FE-2013-03-19.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 6 · 257 reports

- [SDR FDEA201212144302](https://openairdocs.org/sdr/FDEA201212144302.md): Window · cracked · Dec 14, 2012 · N287FE · Boeing 7272D4 · Flight Compartment Windows
  > DURING CRUISE, FL320, PILOTS L1 WINDOW OUTER FRAME CRACKED. MUTIPLE BROWN MARKS ALONG TOP WITH DELAMINATION. COMPLIED WITH QRH, TURNED OFF L1 WINDOW HEAT. INSPECTED WINDOW AND FOUND GLASS PANELS TO BE OK. THE INNER VINYL PANEL IS SEPARATED. 1 "CRACK" STA
- [SDR FDEA201112305461](https://openairdocs.org/sdr/FDEA201112305461.md): Slide · low pressure · Dec 30, 2011 · N287FE · Boeing 7272D4 · Escape Slide
  > ON INBOUND WALK AROUND, FOUND ESCAPE SLIDE PRESSURE GAUGE READING BELOW LIMITS. R & R ESCAPE SLIDE IAW 25-60-015-2. ACFT OK FOR CONT SERVICE.
- [SDR FDEA201112105237](https://openairdocs.org/sdr/FDEA201112105237.md): Indicator · failed · Dec 10, 2011 · N287FE · Boeing 7272D4 · Airspeed/Mach Indicator
  > CAPT AIRSPEED INDICATOR FAILED ON TAKE OFF. PULLED AND RESET CIRCUIT BREAKER, INDICATOR NORMAL. PERFORMED TEST ON DADC-1 AIR SPEED INDICATOR FAILS TEST. R & R CAPT'S AIRSPEED INDICATOR IAW MM 34-12-021-4. OPS CHECKED IAW MM 34-12-000-5-2, 8A. OPS CHECKED NOR
- [SDR FDEA201110224623](https://openairdocs.org/sdr/FDEA201110224623.md): Battery Pack · inoperative · Oct 22, 2011 · N287FE · Boeing 7272D4 · Emergency Lighting
  > FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. R & R ESCAPE SLIDE LIGHT BATTERY PACK REF AMM 33-50-051-2.
- [SDR FDEA201110194595](https://openairdocs.org/sdr/FDEA201110194595.md): Battery Pack · inoperative · Oct 19, 2011 · N287FE · Boeing 7272D4 · Emergency Lighting
  > FORWARD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. R & R ESCAPE SLIDE LIGHT BATTERY PACK. OPS CHECKED NORMAL IAW MM 33-50-051-2.
- [SDR FDEA201108173309](https://openairdocs.org/sdr/FDEA201108173309.md): Control Cable · broken · Aug 17, 2011 · N287FE · Boeing 7272D4 · Trailing Edge Flap Actuator
  > ON CLIMBOUT THRU 20K NOTICED OCCASIONAL VIBRATION IN THE CONTROL COLUMN SPOILERS WERE SLIGHTLY DEPLOYED. NUMEROUS RESETS WITH THE SPOILER HANDLE. SLIGHTLY DEPLOYING SPOILERS DID NOT HELP. ON BLOCK IN DISCOVERED LT INBD FLAP OUTER CABLE BROKEN, ALONG WITH A
- [SDR FDEA201106102198](https://openairdocs.org/sdr/FDEA201106102198.md): Skin · misrepaired · Jun 10, 2011 · N287FE · Boeing 7272D4 · Cargo/Baggage Doors
  > C2 DOOR EXTERIOR SKIN AFT LOWER EDGE HAS FASTENERS WITH IMPROPER SPACING. REMOVED EXISTING REPAIR ANGLE IAW SRM 51-30-2. FABRICATED REPAIR ANGLE, FILLER, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW EA 7-5230-136769.
- [SDR FDEA201106092171](https://openairdocs.org/sdr/FDEA201106092171.md): Skin · gouged · Jun 9, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620 STR 4L. REMOVED DAMAGED UPPER INNER SKIN SECTION, FABRICATED & INSTALLED NEW INNER SKIN IAW SRM 51-30-2, SRM 51-10-2 & SRM 53-10-2 FIG 3A.
- [SDR FDEA201106092170](https://openairdocs.org/sdr/FDEA201106092170.md): Web · cracked · Jun 9, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Structure
  > AFT AIRSTAIRS LT LOWER TORQUE BOX UPPER WEB IS PUNCTURED AND CRACKED AT BS 1225, (BELOW BAZOOKA VALVE STAND-OFF) CUTOUT DAMAGE ON LT LWR TORQUE BOX UPPER WEB IAW SRM REV 103, 51-40-2 FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51
- [SDR FDEA201106062131](https://openairdocs.org/sdr/FDEA201106062131.md): Frame · corroded · Jun 6, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > CORROSION FWD SIDE STA 1166 FRAME STR 21L. REMOVED DAMAGED FRAME SECTION, FABRICATED NEW FRAME SECTION & 2 EA. SPLICES, INSTALLED NEW FRAME IAW SRM 51-30-2, SRM 53-10-2 FIG 5, SRM 51-20-1, SRM 51-10-2 & SRM 51-40-3 FIG 1 AND DWG 65-16549.
- [SDR FDEA201106062133](https://openairdocs.org/sdr/FDEA201106062133.md): Tripler · corroded · Jun 6, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INNER SKIN TRIPLER STA. 1164 STR 21L REMOVED DAMAGED INNER SKIN TRIPLER, FABRICATED & INSTALLED NEW TRIPLER AT BS 1164 IAW SRM 51-10-2, SRM 51-30-2 & DWG 65-25607.
- [SDR FDEA201106062134](https://openairdocs.org/sdr/FDEA201106062134.md): Tee Fitting · damaged · Jun 6, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > C2 DOOR CUTOUT LOWER SECTION, INNER CHORD HAS DOUBLE DRILLED HOLES AND HOLES WITH INSUFFICIENT SPACING AT RBL 21 BETWEEN BS 980- BS 990. REMOVED C2 DOOR CUTOUT FITTING AND TRANSITION FITTING FOR ACCESS AND REMOVED TEE FROM STA 950D TO 1010 IAW SRM 51-30-2.
- [SDR FDEA201106042112](https://openairdocs.org/sdr/FDEA201106042112.md): Skin · dented · Jun 4, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > LT SIDE OF FUSELAGE HAS A DENT AT BS 1260 BETWEEN STRINGER 21L AND 22L. CUTOUT DAMAGE AREA ON LT SIDE OF FUSELAGE BS 1260 BETWEEN STR 21L AND 22L IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3.063 IAW SRM 53-30-3. INSTALLED DOUBLER IAW SRM 53-30-3, FIG 1.
- [SDR FDEA201106012080](https://openairdocs.org/sdr/FDEA201106012080.md): Skin · gouged · Jun 1, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > INNER SURROUND SKIN GOUGED STA 620, STR 16L. REMOVED MCD INNER SURROUND SKIN LOWER SECTION, FABRICATED & INSTALLED NEW INNER LOWER SKIN IAW SRM 51-30-2, SRM 51-10-2 & DWG 53FX1535 & SRM 53-10-2 FIG 3A.
- [SDR FDEA201105312034](https://openairdocs.org/sdr/FDEA201105312034.md): Stringer · corroded · May 31, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27R AT BS 720F. CUTOUT DAMAGED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND SPLICE REPAIR IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1.
- [SDR FDEA201105282014](https://openairdocs.org/sdr/FDEA201105282014.md): Structure · cracked · May 28, 2011 · N287FE · Boeing 7272D4 · Trailing Edge Flaps
  > LEFT I/B FLAP, AFT FLAP I/B TRACK CUTOUT CRACKED. REMOVED MID FLAP LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD IAW SRM 57-50-2 FIG 5 AND 51-30-5. INSTALLED I/B LT MID FLAP CHORD IAW SRM 51-30-2, REV 103
- [SDR FDEA201105241956](https://openairdocs.org/sdr/FDEA201105241956.md): Skin · corroded · May 24, 2011 · N287FE · Boeing 7272D4 · Rudder, Plate/Skin
  > UPPER RUDDER RT SIDE HAS SMALL AREA OF CORROSION ON EXTERIOR SKIN AT TOP OF RUDDER. REMOVED CORROSION ON RH SIDE OF UPPER RUDDER IAW SRM REV 103, 51-10- 6. FABRICATED DOUBLER IAW SRM 55-20-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-20 AND 55-20-3 FIG 1 AND EA
- [SDR FDEA201105241954](https://openairdocs.org/sdr/FDEA201105241954.md): Bulkhead · cracked · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Bulkhead
  > RT WW BS 870, BULKHEAD IS CRACKED BELOW LOAD CONTROL VALVE, (NDT VERIFIED). CUT OUT DAMAGE ON BULKHEAD BELOW LOAD CONTROL VALVE IAW SRM REV 103, 51-10-1. FABRICATED REPAIR DOUBLERS IAW SRM 53-10-9 FIG 5. INSTALLED DOUBLERS IAW SRM 53-10-9 FIG 5.
- [SDR FDEA201105241938](https://openairdocs.org/sdr/FDEA201105241938.md): Frame · cracked · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > FWD CARGO COMPT LOWER STUB FRAME EXTENSION BETWEEN STR 21L-22L AT BS 600 IS CRACKED AT THE LOWER END, IN THE UPPER RADIUS. REMOVED LOWER STUB FRAME AT BS 600, STRINGER 21L-22L IAW B727 SRM 51-30-2. FABRICATED STUB FRAME IAW DRAWING 53FX1350 REV A. INSTALL
- [SDR FDEA201105241939](https://openairdocs.org/sdr/FDEA201105241939.md): Frame · cracked · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > FWD CARGO COMPT. LOWER STUB FRAME EXTENSION BTWN STR 21L-22L AT BS 560 IS CRACKED AT THE LOWER END, IN THE RADIUS. (NDT VERIFIED) REMOVED LOWER STUB FRAME EXTENSION IAW SRM 51-30-2, FABRICATED NEW STUB FRAME IAW DWG 53FX1350, HEAT TREATED STUB FRAME TO -T6 C
- [SDR FDEA201105241953](https://openairdocs.org/sdr/FDEA201105241953.md): Shear Tie · corroded · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 700 (AFT SIDE) BETWEEN STRINGER 28L AND 27L.
- [SDR FDEA201105231937](https://openairdocs.org/sdr/FDEA201105231937.md): Web · cracked · May 23, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA RT TORQUE BOX UPPER LIGHTENING HOLE AT BS 1320 HAS A SMALL CRACK AT EDGE. CUT OUT DAMAGED AREA IAW B727 SRM REV 103 51-40-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 REV 103. INSTALLED DOUBLER IAW SRM 51-30-2 REV 103.
- [SDR FDEA201105231934](https://openairdocs.org/sdr/FDEA201105231934.md): Skin · gouged · May 23, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620 STR 10L. REMOVED DAMAGED MCD INNER SKIN (UPPER AFT) SPLICE, FABRICATED NEW, AND INSTALLED IAW SRM 51-30-2 & SRM 53-10-2 FIG 3A.
- [SDR FDEA201105221927](https://openairdocs.org/sdr/FDEA201105221927.md): Bulkhead · misinstalled · May 22, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Bulkhead
  > BS 1183 PRESSURE BULKHEAD - LBL 17.8 VERT BEAM HAS SEVERAL FASTENERS WITH INSUFFICIENT SPACING. TRIMMED OFF AFT FLANGE AND LOWER END OF 65-16350-299 BEAM, REMOVED EXISTING 65- 16350-284 STRAP. TRIMMED OUT BULKHEAD WEB (3 PLACES) MAINTAINING 0.5" TRIM RADI
- [SDR FDEA201105221928](https://openairdocs.org/sdr/FDEA201105221928.md): Stringer · corroded · May 22, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > STRINGER 28R IS CORRODED AT BS 990. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1 FIG 1 AND STRINGER DRAWING 65-58387, TREATED AND PRIMED IAW SRM 51-10-2
- [SDR FDEA201105221926](https://openairdocs.org/sdr/FDEA201105221926.md): Shear Tie · corroded · May 22, 2011 · N287FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > SHEAR TIE IS CORRODED ON LWR FWD FLANGE AT BS970 BTWN STR 29L - 28L.
- [SDR FDEA201105211924](https://openairdocs.org/sdr/FDEA201105211924.md): Frame · misrepaired · May 21, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > FRAME BS 1090 HAS IMPROPER REPAIR BTWN STR 27L - 28L. REMOVED REPAIR FROM BS 1090 FRAME BETWEEN STR 27L- 28L IAW SRM REV 103, 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3, FIG 1 AND 53-10-2, FIG 5 INSTALLED DOUBLER IAW SRM 51-40-3, FIG. 1.
- [SDR FDEA201105191884](https://openairdocs.org/sdr/FDEA201105191884.md): Door Frame · damaged · May 19, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Structure
  > C-1 DOOR CUTOUT, FWD FRAME BS 560, WEB AND OUTER ANGLE HAVE DRILL DAMAGE AT STR 22R, IN TWO PLACES. REMOVED DAMAGED FRAME WEB, FABRICATED & INSTALLED NEW WEB IAW DWG 65-56100, CUTOUT BS 560 CHORD, FABRICATED REPAIR PARTS & INSTALLED REPAIR IAW EA 7-5310-151200
- [SDR FDEA201105181942](https://openairdocs.org/sdr/FDEA201105181942.md): Web · cracked · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS, RT LOWER TORQUE BOX INBD WEB HAS A CRACK AT EDGE OF UPPER ROW RIVET. CUT OUT DAMAGED AREA IAW SRM REV 103 51-10-1. FABRICATED FILLER & DOUBLER IAW SRM 53-10-2 & 51-40-2 FIG 1. INSTALLED FILLER & DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201105181940](https://openairdocs.org/sdr/FDEA201105181940.md): Web · cracked · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS, RT LWR TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE AT BS 1223, 7 INCHES. CUT OUT DAMAGED AREA IAW SRM REV 103 51-40-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201105181941](https://openairdocs.org/sdr/FDEA201105181941.md): Web · punctured · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR LT LOWER TORQUE BOX UPPER WEB HAS PUNCTURE HOLE AT STAND-OFF BRACKET. CUT OUT DAMAGE IAW SRM REV 103 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG1 REV 103. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201105182015](https://openairdocs.org/sdr/FDEA201105182015.md): Stringer · corroded · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L IS CORRODED WITH EXFOLIATION BETWEEN BS 970-990. REMOVED SECTION OF STRINGER 27L BETWEEN BS 970 AND 990 IAW SRM 53-10-3 FIG 1. FABRICATED FILLER AND STRINGER SECTION IAW SRM 53-10-3 FIG 1. INSTALLED FILLER AND REPAIR SECTION IAW SRM 53-10-3 F
- [SDR FDEA201007142508](https://openairdocs.org/sdr/FDEA201007142508.md): Element · inoperative · Jul 14, 2010 · N287FE · Boeing 7272D4 · Overheat Detection
  > AT FL 350 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH EMERGENCY PROCEDURE WHICH REQUIRES TURNING OFF RT PACK, WITH ONLY THE LT PACK ON ACFT WOULD NOT MAINTAIN CABIN ALTITUDE. WE HAD TO DECEND TO 11,000 FT TO GET CABIN ALT TO 9,500 FT. R & R R
- [SDR FDEA200902120513](https://openairdocs.org/sdr/FDEA200902120513.md): Skin · damaged · Feb 12, 2009 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN DAMAGE FROM STA 560 TO 580 STRINGER'S 27L TO 28R REPAIRED SKIN DAMAGE FROM STA 560 TO 580 STRINGERS 27L TO 28R IAW EA NR 7-5330-126895, FUSELAGE SKIN DENTS BETWEEN BS 560 AND 580 STR 27L AND 28R REPAIR.
- [SDR FDEA200812185195](https://openairdocs.org/sdr/FDEA200812185195.md): Control Lever · loose · Dec 18, 2008 · N287FE · Boeing 7272D4 · Trailing Edge Flap Control System
  > FLIGHT TEST OUTBOARD FLAP GAUGE INDICATED BETWEEN 20 DEGREES AND 25 DEGREES AT FLAPS 25 DEGREES AND BETWEEN 25 INCH AND 30 INCH AT FLAPS 30 INCH ALL OTHER POSITIONS OK (REPEAT) PERFORMED ADJUSTMENT AND TEST ON OTBD T/E FLAP POSITION TRANSMITTER REF MM 27-52-01
- [SDR FDEA200812125131](https://openairdocs.org/sdr/FDEA200812125131.md): Floorbeam · cracked · Dec 12, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Floor Beam
  > ANGLE FOR FLOOR JUST FWD OF FLIGHT DECK DOOR CUT OUT IS CRACKED REMOVED FLOOR SUPPORT AND ATTACH BRACKET, FABRICATED DRILLED, TRIMMED, TREATED AND PRIMED NEW ATTACH ANGLE. INSTALLED FLOOR SUPPORT AND NEW ANGLE. REFERENCE BOEING DWG NR 65-17593/ITEM NR -239
- [SDR FDEA200812065095](https://openairdocs.org/sdr/FDEA200812065095.md): Angle · corroded · Dec 6, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > LWR EXTERIOR FUSELAGE BS 740, LBL6 TO LBL 10, WL 148.5 TO WL 150 JUST AFT OF GROUND A/C HOOK UP DUCT CORRODED REMOVED PANEL, A/C DUCT AND BODY FAIRING, AND HYD LINES FOR ACCESS REF SRM 51-30-02. REMOVED AND FABRICATED L ANGLE AND INSTALLED NEW L ANGLE REF
- [SDR FDEA200812055089](https://openairdocs.org/sdr/FDEA200812055089.md): Bracket · cracked · Dec 5, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach Fittings
  > RADAR R/T SHELF TRAY CRACKED AT AFT RT AND LT FOOT REMOVED AND REPLACED RT SHELF REF SRM 51-30-02.
- [SDR FDEA200812025041](https://openairdocs.org/sdr/FDEA200812025041.md): Angle · corroded · Dec 2, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > EXTERIOR LWR FUSELAGE INSIDE DELTA BEAM BS 740 LBL5 TO RBL 5 WL 148.5 LOWER ANGLE UPPER SURFACE CORRODED. REMOVED AND REPLACED T-ANGLE REF SRM 51-30-2 ORIGINAL MATERIAL THICKNESS.125. REMOVED.025 MATERIAL REMAINING.100 OUT OF LIMITS REF SRM 53-10-1 FIG 1.
- [SDR 08FDEA04968](https://openairdocs.org/sdr/08FDEA04968.md): Rib · cracked · Nov 24, 2008 · N287FE · Boeing 7272D4 · Wing, Rib/Bulkhead
  > LT WING L/E RIB LWR CHORD HAS 2 CRACKS AT 5 INCH AND 18 INCH FROM SPAR, FSS 122. REMOVED PNL 6301 TO FOM. FABRICATED ANGLE REF DWG 64-8342-19 DRILLED-UP, TREATED, PRIMED, AND INSTALLED ANGLE REF SRM 51-30-5, MM 51-20-021, MM 51-20-051, AND SRM 51-30-2. INST
- [SDR 08FDEA04964](https://openairdocs.org/sdr/08FDEA04964.md): Skin Panel · cracked · Nov 24, 2008 · N287FE · Boeing 7272D4 · Wing, Plate/Skin
  > WHILE ACCOMPLISHING "OK TO WORK" STEP ON SNRM (N00791)) FOUND WING L/E SKIN CRACKED (LT WING) AT FSS 122, LWR SURFACE OF SKIN. REMOVED AND REINSTALLED ANTI-ICE DUCT (LT L/E WING ROOT) REF MM 36-00-001-2, LEAK CHECK GOOD. REPAIRED CRACK REF SRM 57-30-4 FIG 8.
- [SDR 08FDEA04960](https://openairdocs.org/sdr/08FDEA04960.md): Bracket · corroded · Nov 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > RT MLG W/W CUTOUT SEAL BEAM (STR 19R), AREAS OF CORROSION ON TOP SIDE OF BEAM FROM FS 906 TO FS 930, RBL 74, WL 105 REMOVED CORROSION FROM BRACKET, STA 920 ORIG T.094, REMAINING T.071,.023 MATERIAL LOSS OUT OF LIMITS. REPLACED BRACKET STA 920. REMOVED CO
- [SDR 08FDEA04947](https://openairdocs.org/sdr/08FDEA04947.md): Panel · punctured · Nov 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT, PFM BOX, PUNCTURE JUST BELOW PFM DOOR REPAIRED PUNCTURE IN PFM BOX REF SRM 51-40-20 PAR'S 7, 14, 15, 19, 20, AND FIG'S 8, 211, SRM 51-20-4 AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA04927](https://openairdocs.org/sdr/08FDEA04927.md): Stringer · corroded · Nov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > AFT PIT S27L LONGERON/FITTING HAS CORROSION AT BS 1130 REMOVED FASTENERS, REMOVED CORROSION, NDT (HFEC) BLENDOUT AREA AND FASTENER HOLES. ALODINED AND CIC, D AREA. WITH NO LIMITS REF EA 7-5310-123810, THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA04924](https://openairdocs.org/sdr/08FDEA04924.md): Channel · cracked · Nov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > RADAR R/T SHELF, RT SIDE HAT CANNEL ON UPPER SIDE OF SHELF IS CRACKED. REPLACED RT SIDE HAT CHANNEL ON RADAR R/T SHELF IN ACCORDANCE WITH BOEING DRAWING 65C16129 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR
- [SDR 08FDEA04923](https://openairdocs.org/sdr/08FDEA04923.md): Stiffener · corroded · Nov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > LT MLG WHEEL WELL APU AIR INLET MOUNT FLANGES CORRODED REMOVED CORROSION REF SRM 51-10-1 ORIGINAL THICKNESS.150', REMOVED.018', REMAINING THICKNESS,.132' OUT OF LIMITS REF SRM 53-10-1 FIG 1. REPLACED 323 STIFFENER REF DWG 65-18636, AND SRM 51-30-2 PG 1-10.
- [SDR 08FDEA04919](https://openairdocs.org/sdr/08FDEA04919.md): Frame Splice · damaged · Nov 19, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > AFT CARGO PIT STATION 1030 FRAME SPLICE AT APPROX STRINGER 24L IS DAMAGED. REPLACED FRAME SPLICE REF SRM 51-30-02 AND DRAWING 69-47200. THIS IS CLASSIFIED AS A MAJOR REPAIR
- [SDR 08FDEA04913](https://openairdocs.org/sdr/08FDEA04913.md): Frame · dented · Nov 18, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > AFT CARGO PIT STATION 1050 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED DAMAGE ON STA 1050 AT STR 26R. REF SRM 51-40-05 PG1 FABRICATED AND INSTALLED DOUBLER FOR FRAME. REF SRM 51-20-1 PG 1 SRM 51-30-02 PG 1-12 FABRICATED AND INSTALLED NEW END ATTACH ANGLE FOR I
- [SDR 08FDEA04912](https://openairdocs.org/sdr/08FDEA04912.md): Frame · dented · Nov 18, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > AFT CARGO PIT STATION 1030 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED FRAME DAMAGE STA 1030 STR 26L REF SRM 51-40-3 FIG 1 PGS 1-6. FORMED DOUBLER REF SRM 51-20-1 PG 1 HEAT TREAT DOUBLER TRACKING 2008-11-129. REMOVED INTERCOSTAL STA 1030, INSTALALED INTERC
- [SDR 08FDEA04911](https://openairdocs.org/sdr/08FDEA04911.md): Frame · dented · Nov 18, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > AFT CARGO PIT STATION 1010 FUSELAGE FRAME DAMAGED AT STRINGER 26L. REPAIRED FRAME REF SRM 51-40-03 FIG1 AND FABRICATED CHANNEL ANGLE REF DWG 65-84827-8 SRM 51-30-02 PG 1-5

Next page: https://openairdocs.org/deregistered/N287FE-2013-03-19/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 = 'N287FE' AND deregistration_id = 'N287FE-2013-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N287FE-2013-03-19/reports

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