# Service difficulty reports: N287SC, cancelled Apr 24, 2017

A list on [N287SC, cancelled Apr 24, 2017](https://openairdocs.org/deregistered/N287SC-2017-04-24.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 4 · 161 reports

- [SDR C8GA20120406005](https://openairdocs.org/sdr/C8GA20120406005.md): Generator · failed · Apr 3, 2012 · N287SC · Boeing 7272A1 · AC Generator-Alternator
  > AFTER TAKEOFF, ALL COCKPIT LIGHTS FLICKERED FOLLOWED BY NR 2 GENERATOR OVER EXCITATION FOLLOWED BY PHASE IMBALANCE. NR 3 BUSS TIE TRIPPED FOLLOWED BY NR 3 GEN I TRIP. TROUBLESHOOTING FOUND NR 3 GENERATOR IS CAUSING THE PROBLEM. DISCONNECTED NR 3 GENERATOR.
- [SDR C8GA20120321004](https://openairdocs.org/sdr/C8GA20120321004.md): Floorbeam · corroded · Mar 20, 2012 · N287SC · Boeing 7272A1 · Fuselage Main, Floor Beam
  > DURING 18 MONTH CPCP INSPECTION, CORROSION WAS FOUND ON OTBD END OF LT FLOORBEAM AT FS 910, AND WL 70. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-08 AND EO 2287-5304.
- [SDR C8GA2011000009](https://openairdocs.org/sdr/C8GA2011000009.md): Relay · inoperative · Jun 30, 2011 · N287SC · Boeing 7272A1 · Global Positioning System
  > DURING CLIMB OPERATION THE FO'S CDI NEEDLE DID NOT DEVIATE WITH COURSE CHANGES WITH THE VOR SELECTED. ALSO, THE CAPTAINS CDI WAS UNREADABLE ON LOCALIZER, SHOWED FROZEN, CENTERED THEN RAPIDLY MOVED LT OF COURSE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED
- [SDR FOTR2102212390](https://openairdocs.org/sdr/FOTR2102212390.md): Skin · debonded · Mar 18, 2011 · N287SC · Boeing 7272A1 · Spoilers
  > RT WING T/E NR 11 SPOILER UPPER SKIN IS DEBONDED OTBD END. REMOVED DAMAGED AREA DIM 10" X 6.25" IAW SRM 51-40-20 PARA 7,11,14,15 AND FABRICATED FILLER DIM 10" X 6.25" AND DOUBLER DIM 12" X 8" FROM 7075T6.025 PO 90010605 IAW SRM 57-50-6 PAGE 14, ITEM 4 AND 51
- [SDR FOTR2102212391](https://openairdocs.org/sdr/FOTR2102212391.md): Skin · debonded · Mar 18, 2011 · N287SC · Boeing 7272A1 · Spoilers
  > RT WING T/E NR 13 SPOILER UPPER SKIN IS DISBONDED. REMOVED DAMAGED AREA DIM 12" X 7.75" IAW SRM 51-40-20, PARA 7,11,14,15 AND FABRICATED FILLER DIM 12" X 7.75" AND DOUBLER DIM 13.5" X 9.25" FROM 7075T6.025 PO 90010605 IAW SRM 57-50-6, PAGE 14, 17 AND 51-40-2
- [SDR FOTR2102212508](https://openairdocs.org/sdr/FOTR2102212508.md): Skin · debonded · Mar 18, 2011 · N287SC · Boeing 7272A1 · Elevator, Plate/Skin
  > RT ELEVATOR TAB T/E IS DISBONDED. REMOVED DAMAGED AREA DIM 6.5" X 6.5" IAW SRM 51-40-20, PAGE 12-14, PARA 7. FABRICATED REPAIR FILLER 6.5" X 6.5" AND DOUBLER DIM 10.5" X 6.5" USING 2024T3 PO 9003621 IAW SRM 51-40-20, PAGE 14-16, PARA 8 AND SRM 55-20-2, PAGE
- [SDR FOTR2102212576](https://openairdocs.org/sdr/FOTR2102212576.md): Tab · debonded · Mar 15, 2011 · N287SC · Boeing 7272A1 · Aileron Tabs
  > LT OTBD AILERON TAB HAS DISBOND ON INBD END. REMOVED DAMAGE ON AILERON INBD END DIM 7" X 3" IAW SRM 51-40-20, PAGE 12, PARA 7. FABRICATED REPAIR CORE IAW SRM 51-40-20, PAGE 14, PARA 8. USING DUR-5052-44-3/16 PO 9009476 DIM 7" X 3". BONDED CORE IAW SRM 51-4
- [SDR FOTR2102212575](https://openairdocs.org/sdr/FOTR2102212575.md): Tab · debonded · Mar 15, 2011 · N287SC · Boeing 7272A1 · Aileron Tabs
  > LT OTBD AILERON TAB HAS DISBOND ON OTBD END. REMOVED DAMAGE ON AILERON TAB DIM 2" X 2" IAW SRM 51-40-20, PAGE 12, PARA 7. FABRICATED REPAIR CORE IAW SRM 51-40-20, PAGE 14, PARA 8 USING DUR-5052-44-3/16 PO 9009476 DIM 2" X 2". BONDED CORE IAW SRM 51-40-20 PA
- [SDR FOTR2102212307](https://openairdocs.org/sdr/FOTR2102212307.md): Spar · cracked · Mar 15, 2011 · N287SC · Boeing 7272A1 · Wing Spar
  > NR 1 SLAT ACTUATOR OTBD MOUNT SUPPORT ON LT WING FRONT SPAR CRACKED. REMOVED CRACKED WEB FROM L/E LT WING SLAT STA 398.1 IAW SRM 51-30-2. FABRICATED NEW WEB FROM 7075T6.063 PO 9009533 DIM 4.5" X 9" IAW SB 727-57-0130 FIG 1. INSTALLED REPAIR WEB IAW SB 727-
- [SDR FOTR2102212335](https://openairdocs.org/sdr/FOTR2102212335.md): Tab · debonded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Aileron Tabs
  > LT WING OTBD AILERON TAB IS DISBONDED AT 4 EA PLACES. REMOVED DAMAGED ON LT OTBD AILERON TAB 30" FROM OTBD END, DIM 7" X 4" IAW SRM 51-40-20-PAGE 12, PARA 7. FABRICATED REPAIR CORE IAW SRM 51-40-20, PAGE 14, PARA 8, USING DUR-5052-44-3/16-N-E ALUMINUM CORE PO
- [SDR FOTR2102212574](https://openairdocs.org/sdr/FOTR2102212574.md): Tab · debonded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Aileron Tab Control System
  > LT OTBD AILERON TAB HAS DISBOND ON UPPER SURFACE 15" FROM OTBD END. REMOVED DAMAGED ON LT OTBD AILERON TAB, FABRICATED REPAIR CORE, BONDED REPAIR CORE, FABRICATED DOUBLER, BONDED DOUBLER, CLEANED, SEALED AND FINISH REPAIR ALL, IAW SRM 51-40-20 WEIGHT AND BALA
- [SDR FOTR2102212539](https://openairdocs.org/sdr/FOTR2102212539.md): Skin · debonded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT INBD MID FLAP T/E UPPER OTBD END HAS AREA DISDOND. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA NR 7, REPAIRED RT INBD MID-FLAP T/E WEDGE BY HOT BONDING REPAIR IAW SRM 51-40-20, PAR NR 20.
- [SDR FOTR2102212489](https://openairdocs.org/sdr/FOTR2102212489.md): Skin · debonded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Spoilers
  > RT WING NR 11 SPOILER UPPER SKIN IS DISBONDED INBD END. REMOVED DAMAGED, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, FABBED REPAIR PARTS, 2 PCS, 1 FILLER 10.75" X 7.0", DOUBLER 12" X 8.5" FROM 7075T6,.025, IAW SRM 51-40-20, CLEANED, SEALED AND FINISHE
- [SDR FOTR2102212487](https://openairdocs.org/sdr/FOTR2102212487.md): Wedge · debonded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > LT INBD FLAP T/E WEDGE, UPPER INBD END IS DISBONDED. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA NR7, REPAIRED LT INBD MID FLAP T/E WEDGE BY OT BONDING DOUBLER IAW SRM 51-40-20, PARA NR 20.
- [SDR FOTR2102212485](https://openairdocs.org/sdr/FOTR2102212485.md): Wedge · debonded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT INBD MID FLAP T/E WEDGE, LWR INBD NR 1 TRACK IS DISBONDED. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20 PARA NR 7, REPAIRED RT INBD MIDFLAP T/E WEDGE LWR NR 1 TRACK AREA BY HOT BONDING REPAIR IAW SRM 51-40-20, PARA NR 20.
- [SDR FOTR2102212402](https://openairdocs.org/sdr/FOTR2102212402.md): Skin · gouged · Mar 14, 2011 · N287SC · Boeing 7272A1 · Leading Edge Devices
  > RT WING NR 5 SLAT T/E SKIN BY INBD HOOK IS GOUGED. CLEANED AREA ON NR 5 SLAT IAW MM12-40-00, FOUND AREA OF GOUGE TO BE OUT OF LIMITS IAW SRM 57-50-1, FIG 2. FRABRICATED REPAIR PLATE FROM 7075-T6,.125 PO 90095-66, MEA 6.5 X 3.1885 IAW SRM 57-50-3, INSTALLED D
- [SDR FOTR2102212361](https://openairdocs.org/sdr/FOTR2102212361.md): Seat Track · corroded · Mar 14, 2011 · N287SC · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > BL-O-SEAT TRACK CORRODED STA 610. REMOVED BL-O- SEAT TRACK STA 590-730 IAW SRM 51-30-2 FABRICATED NEW SEAT TRACK FROM 40456, 7178T6511 PO 9007703 DIM 120" IAW SRM 51-10-2, 51-30-5. INSTALLED SEAT TRACK IAW SRM 51-30-2.
- [SDR FOTR2102212349](https://openairdocs.org/sdr/FOTR2102212349.md): Skin · damaged · Mar 14, 2011 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > DRILL STARTS IN FUSELAGE AT STR 2R STA 400. FOUND AREA TO HAVE A SMALL DELAMINAION ON TEAR STRAP AT STR 2R-3R, L1 =.5 PERCENT = 5 PERCENT, FOUND TO BE WITHIN LIMITS, IAW SRM 53-30-4, FIG 7. INSTALLED RIVETS IAW SRM 51-10-2, 53-30-4.
- [SDR FOTR2102212339](https://openairdocs.org/sdr/FOTR2102212339.md): Skin · cracked · Mar 14, 2011 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > LT WING OTBD FLAP, AFT FLAP HAS CRACK AT L/E, JUST INBD OF MOST OTBD TRACK. CUT OUT DAMAGED AREA DIM 1.2" X 1" ON LT WING OTBD FLAP L/E IAW SRM 57-50-4, FIG 9. FABRICATED REPAIR DOUBLER FROM 2024T3.040 PO 90011142, DIM 7.1" X 7.3" AND FILLER DIM 1.2" X 1" FR
- [SDR FOTR2102212322](https://openairdocs.org/sdr/FOTR2102212322.md): Fence · cracked · Mar 14, 2011 · N287SC · Boeing 7272A1 · Leading Edge Devices
  > 4 SLAT FENCE CRACKED LWR DRAIN HOLE SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-9 PARA. 7. APPLIED REPAIR TO PREPPED AREA IAW SRM 51-40-9, PARA 7 AND REFINISHED SURFACE OF REPAIR IAW SRM 51-40-9, PARA 7.
- [SDR FOTR2102212315](https://openairdocs.org/sdr/FOTR2102212315.md): Skin · cracked · Mar 14, 2011 · N287SC · Boeing 7272A1 · Leading Edge Devices
  > NR 2 SLAT LWR SKIN CRACKED AT INBD TRACK TO SKIN ATTACH FASTENERS. CUT OUT DAMAGED AREA DIM 3.3" X 5.55" IAW SRM 57-50-3, FIG 1. FABRICATED REPAIR DOUBLER FROM 7075T6.080 PO 90011142 DIM 6.75" X 7.4" AND FILLER FROM 7075T6.080 PO90011142 DIM 5.55" X 3.3"
- [SDR FOTR2102212546](https://openairdocs.org/sdr/FOTR2102212546.md): Skin · dented · Mar 14, 2011 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > EVALUATE EXISTING DENT ON FUSELAGE SKIN AT BS 1336 ABOVE STRINGER 26L. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1, FIG 1, DETAIL 2. DEBONDED AND REBONDED SKIN IAW SRM 51-20-4, REMOVED DAMAGED AREA IAW SRM 51-40-2, FABRICATED REPAIR DOUBLER
- [SDR C8GA201000009](https://openairdocs.org/sdr/C8GA201000009.md): Bushing · defective · Apr 16, 2010 · N287SC · Boeing 7272A1 · Landing Gear Doors
  > FLT 716 FROM CVG TO MEM. WHILE CLIMBING THROUGH 15,000 FEET ACCELERATING THROUGH 280 KTS A HIGH FREQUENCY AERODYNAMIC VIBRATION DEVELOPED. CREW WAS UNABLE TO IDENTIFY THE SOURCE. AIRCRAFT RETURN TO KCVG WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECT
- [SDR C8GA20090179](https://openairdocs.org/sdr/C8GA20090179.md): Actuator · leaking · Aug 19, 2009 · N287SC · Boeing 7272A1 · Leading Edge Slat Actuator
  > DURING CLIMB OPERATION A TOTAL "A" HYD SYS FAILURE OCCURRED. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE NR 3 SLAT ACTUATOR INBD FITTING WAS CRACKED. REMOVED AND REPLACED THE NR 3 SLAT ACTUATOR, REMOVED
- [SDR C8GA20090133](https://openairdocs.org/sdr/C8GA20090133.md): Actuator · leaking · Aug 4, 2009 · N287SC · Boeing 7272A1 · Leading Edge Slat Actuator
  > FLT 721 FROM TOL TO ROC. AFTER DEPARTING THE RUNWAY THE GEAR WOULD NOT RETRACT, A LOSS OF SYSTEM "A" HYDRAULICS WAS NOTED. THE AIRCRAFT RETURNED TO TOL WHERE AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT
- [SDR C8GA20090076A](https://openairdocs.org/sdr/C8GA20090076A.md): Door · unsecure · May 22, 2009 · N287SC · Boeing 7272A1 · Passenger/Crew Doors
  > FLT 711 FROM SAN TO PHX. DURING CLIMB OPERATION A LOSS OF CABIN PRESSURE CONTROL WAS EXPERIENCED FOLLOWED BY AN AFT ENTRY DOOR LIGHT. THE AIRCRAFT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT IN PHX. POST FLIGHT INSPECTION WAS PERFORMED. THE AFT ENTRY DOO
- [SDR C8GA20090062](https://openairdocs.org/sdr/C8GA20090062.md): Latch · dirty · Apr 23, 2009 · N287SC · Boeing 7272A1 · Cargo/Baggage Doors
  > FLT 1738- DURING CRUISE OPERATION THE MAIN CARGO DOOR RED LIGHT ILLUMINATED, ON BULKHEAD BOTH VENT DOOR AND HOOK UNLOCKED LIGHTS WERE ILLUMINATED. POST FLIGHT INSPECTION WAS PERFORMED. CLEANED AND LUBRICATED DOOR LATCHES AND SWITCHES. OPERATIONAL AND PRESSU
- [SDR C8GA20090136](https://openairdocs.org/sdr/C8GA20090136.md): Skin · cracked · Mar 23, 2009 · N287SC · Boeing 7272A1 · Spoilers
  > WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 11 SPOILER PANEL IS DELAMINATED AT UPPER T/E. REMOVED DAMAGED AREA DIM. 5" X 2", FABRICATED FILLER FROM 2024 T3.025" DIM 5" X 2" AND FABRICATED DOUBLER FROM 2024 T3.025" DIM. 9" X 4".
- [SDR C8GA20090135](https://openairdocs.org/sdr/C8GA20090135.md): Panel · cracked · Mar 23, 2009 · N287SC · Boeing 7272A1 · Spoilers
  > WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 9 SPOILER PANEL IS DELAMINATED AT UPPER O/B SURFACE. REMOVED DAMAGED AREA DIM. 5" X 2", FABRICATED FILLER FROM 2024 T3.025" DIM 5" X 2" AND FABRICATED DOUBLER FROM 2024 T3.025" DIM. 9
- [SDR C8GA20090134A](https://openairdocs.org/sdr/C8GA20090134A.md): Support Angle · cracked · Mar 23, 2009 · N287SC · Boeing 7272A1 · Wing Miscellaneous Structure
  > WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE # 6 SLAT I/B & O/B ROD END SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED I/B & O/B RIBS AT # 6 SLAT WS 530. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090137A](https://openairdocs.org/sdr/C8GA20090137A.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Spoilers
  > WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 12 SPOILER PANEL IS DELAMINATED AT I/B UPPER SURFACE. REMOVED DAMAGED AREA DIM. 2" X 2", FABRICATED FILLER FROM 2024 T3.025" DIM 2" X 2" AND FABRICATED DOUBLER FROM 2024 T3.025" DIM.
- [SDR C8GA20090132](https://openairdocs.org/sdr/C8GA20090132.md): Tab · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Aileron Tabs
  > WHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT IB AILERON TAB PREVIOUS REPAIR IS DELAMINATED. CUT OUT DAMAGED AREA DIM 5" X 9", FABRICATED REPAIR FILLER FROM 2024 T3.012" DIM 5" X 9" AND DOUBLER FROM 2024 T3.012" DIM. 6" X 12". INSTALLED REPAI
- [SDR C8GA20090131](https://openairdocs.org/sdr/C8GA20090131.md): Skin · canning · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT FUSELAGE SKIN AT BS 670 STRINGER 26R HAS OIL CANNING. CUT OUT DAMAGED AREA DIM 2.250" X 2.750", FABRICATED REPAIR DOUBLER FROM 2024 T3.080 DIM 10.375 X 7.250" AND FILLER FROM 2024 T3.071" DIM. 10.3
- [SDR C8GA20090130](https://openairdocs.org/sdr/C8GA20090130.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD AFT FLAP IS CRACKED AT EDGE WBL 124. REMOVED DAMAGED SKIN AND CORE DIM 7" X 1.5", FABRICATED REPAIR CORE DIM 7" X.5" FROM 5052-44-3/16 AND 2 EA DOUBLER'S FROM 2024 T3.016" DIM 5" X 3", 8.5" X 3". HOT BON
- [SDR C8GA20090129](https://openairdocs.org/sdr/C8GA20090129.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD FLAP IS DELAMINATED ON THE LWR T/E. REMOVED DAMAGE AREA, FABRICATED DOUBLER. HOT BONDED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090128](https://openairdocs.org/sdr/C8GA20090128.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD FOREFLAP IS DELAMINATED ON THE LWR SURFACE NEAR THE INBD END. REMOVED LT INBD FOREFLAP, REMOVED DAMAGE AREA DIM 5" DIA. CIRCLE. FABRICATED DOUBLER FROM 2024 T3.016". HOT BONDED REPAIR, NO OTHER DEFECTS WE
- [SDR C8GA20090127](https://openairdocs.org/sdr/C8GA20090127.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > WHILE IN HEAVY MX IT WAS NOTED THAT LT WING OTBD MID-FLAP HAS AN AREA OF DELAMINATION ON THE T/E OTBD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090126](https://openairdocs.org/sdr/C8GA20090126.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Trailing Edge Flaps
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING OTBD MID-FLAP HAS AREA OF DELAMINATION ON T/E ON OTBD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090125](https://openairdocs.org/sdr/C8GA20090125.md): Stringer · gouged · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX IT WAS NOTED THAT STRINGER 22L AT STA 1180 HAS A GOUGE ON THE UPPER FLANGE. REMOVED EXISTING STRINGER SPLICE AND FABRICATED NEW STRINGER AND SPLICE. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090124](https://openairdocs.org/sdr/C8GA20090124.md): Skin · damaged · Mar 23, 2009 · N287SC · Boeing 7272A1 · Nacelle/Pylon, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT NR 1 AND NR 3 PYLON UPPER SURFACE FASTENERS G AND H ARE PULLED THRU THE PANEL AT ENGINE STA 146 BBL 68. REMOVED PANELS AND FABRICATED NEW PANELS. INSTALLED NEW PANELS. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SE
- [SDR C8GA20090123](https://openairdocs.org/sdr/C8GA20090123.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 1179 BETWEEN STR. 20L-23R IS NON-COMPLIANT WITH SRM. THE EXISTING REPAIR WAS REMOVED, HFEC WAS PERFORMED WITH NO DEFECTS. FABRICATED DOUBLER FROM 2024 T3.071" DIM 18.3" X 11.3",
- [SDR C8GA20090122](https://openairdocs.org/sdr/C8GA20090122.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 720A +12 BETWEEN STR. 27L-27R IS NON-COMPLIANT WITH SRM. EXISTING REPAIR WAS REMOVED, HFEC WAS PERFORMED WITH NO DEFECTS. FABRICATED DOUBLER FROM 2024 T3.100 INCH DIM 30.25 INCH
- [SDR C8GA20090121](https://openairdocs.org/sdr/C8GA20090121.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Spoilers
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE NR 11 SPOILER OTBD END T/E IS DELAMINATED. DAMAGED AREA WAS REMOVED. FABRICATED REPAIR FILLER, AND REPAIR DOUBLER, INSTALLED BOND REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090120](https://openairdocs.org/sdr/C8GA20090120.md): Skin · delaminated · Mar 23, 2009 · N287SC · Boeing 7272A1 · Spoilers
  > WHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 12 SPOILER I/B END IS DELAMINATED. DAMAGED AREA WAS REMOVED. FABRICATED REPAIR FILLER, AND REPAIR DOUBLER, INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090119](https://openairdocs.org/sdr/C8GA20090119.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 720B +11 BETWEEN STRINGERS 26R-28R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSPECTION WITH NO DEFECTS. FABRICATED AND INSTALLED TIPPLER FROM 2024 T3.07
- [SDR C8GA20090118](https://openairdocs.org/sdr/C8GA20090118.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT THE LOWER FWD CORNER ON THE R2 DOOR CUTOUT IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED TIPPLER FROM 2024 T3.071
- [SDR C8GA20090117](https://openairdocs.org/sdr/C8GA20090117.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT R2 DOOR CUTOUT IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED TIPPLER FROM 2024T3.100" DIM 20" X 21, DOUBLER FROM 2
- [SDR C8GA20090116](https://openairdocs.org/sdr/C8GA20090116.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 1188 STRINGER 21L - 22L IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSPECTION WITH NO DEFECTS. FABRICATED AND INSTALLED NEW DOUBLER FROM 2024 T3.071" DIM
- [SDR C8GA20090115](https://openairdocs.org/sdr/C8GA20090115.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 297 STRINGER 22R -24R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED NEW FILLER FROM 2024 T3.040" DIM 17.750" X
- [SDR C8GA20090114](https://openairdocs.org/sdr/C8GA20090114.md): Skin · misrepaired · Mar 23, 2009 · N287SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 342 STRINGER 23R -25R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED NEW FILLER FROM 2024 T3 DIM 20.5" X 11" AND

Next page: https://openairdocs.org/deregistered/N287SC-2017-04-24/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 = 'N287SC' AND deregistration_id = 'N287SC-2017-04-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N287SC-2017-04-24/reports

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