# Service difficulty reports: Boeing 727-2A1

A list on [Boeing 727-2A1](https://openairdocs.org/model/boeing-727-2a1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 502 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 C8GA2011000001](https://openairdocs.org/sdr/C8GA2011000001.md): Control Cable · out of adjust · Mar 23, 2011 · N286SC · Boeing 7272A1 · Landing Gear Retraction/Extension System
  > DURING APPROACH, WITH THE GEAR LEVER PLACED IN THE DOWN POSITION, THE GREEN LANDING GEAR INDICATION LIGHTS WERE ILLUMINATED AS WELL AS THE RED INDICATION LIGHTS ON THE FWD PANEL AND THE ENGINEERS PANEL. THE LANDING GEAR WAS CYCLED WITH THE SAME INDICATIONS, A
- [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 FOTR20006NR2095](https://openairdocs.org/sdr/FOTR20006NR2095.md): Skin · dented · Feb 24, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > (FOTR) DENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006. N/R 02095- R & R PREVIOUS REPAIR TO LT FUSELAGE SKIN AT STA 1319 STR 9L IAW SRM 53-30-3 FIG 1, REV 102. MATERIAL USED: 2024-T3, 0.063", DIM: 9.250" X 8.750".
- [SDR FOTR20006NR2059](https://openairdocs.org/sdr/FOTR20006NR2059.md): Skin · debonded · Feb 13, 2010 · N286SC · Boeing 7272A1 · Aileron Tabs
  > RT WING INBD AILERON TAB LOWER SURFACE DISBONDED 22 INCHES FROM OTBD END. REPAIRED ON FASI WO 20006, N/R 02059. REPAIRED RT WING INBD AILERON TAB AT WBL 280 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: FILLER- 2024-T3, 0.010, DIM: 4.
- [SDR FOTR20006NR2054](https://openairdocs.org/sdr/FOTR20006NR2054.md): Structure · cracked · Feb 12, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT WING INBD MID FLAP LOWER T/E CHORD CRACKED WBL 100. REPAIRED ON FASI WO 20006, N/R 02054. REMOVED AND REPLACED RT WING INBD MID-FLAP LOWER T/E CHORD SECTION AT WS 100.0 IAW B727 SRM 51-30-5 AND 57-50-2, FIG 5, REV 102. MATERIAL USED: BAC1503-10046 7075-T
- [SDR FOTR20006NR2033](https://openairdocs.org/sdr/FOTR20006NR2033.md): Skin · debonded · Feb 10, 2010 · N286SC · Boeing 7272A1 · Spoilers
  > RT WING NR 9 SPOILER LOWER SURFACE HAS DISBONDED DOUBLER JUST AFT OF ACTUATOR ATTACH FITTING. REPAIRED ON FASI WO 20006, N/R 02033. REPAIRED RT WING NR 9 SPOILER LOWER SURFACE AT WBL 113 BY HOT BY 8.0.
- [SDR FOTR20006NR2031](https://openairdocs.org/sdr/FOTR20006NR2031.md): Skin · debonded · Feb 10, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > LT INBD AFT FLAP LOWER SURFACE HAS DISBONDED AREA AT WBL 135. REPAIRED ON ASI WO 20006, N/R 02031. INSTALLED HOT BONDED REPAIR TO LEFT INBD AFT FLAP LOWER SURFACE AT WBL 135 IAW B727 SRM 51-40-20, PARA 20 AND 51-40-23, REV 102. MATERIAL USED: CORE; 5052-4.4-
- [SDR FOTR20006NR2028](https://openairdocs.org/sdr/FOTR20006NR2028.md): Skin · punctured · Feb 10, 2010 · N286SC · Boeing 7272A1 · Elevator, Plate/Skin
  > RT ELEVATOR LOWER SKIN WORN THRU AT ELEV STA 78 NEAR CENTER OF ELEVATOR. REPAIRED ON FASI WO 20006, N/R 02028. INSTALLED REPAIR DOUBLER ON RIGHT ELEVATOR LOWER SURFACE AT ELEV STA 78, IAW B727 SRM 55-20-3 FIG 4, REV 102. MATERIAL USED: 2024-T3, DIM; 4.325 B
- [SDR FOTR20006NR2027](https://openairdocs.org/sdr/FOTR20006NR2027.md): Frame · damaged · Feb 9, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > UPPER CABIN FRAME DAMAGED AT BS 380 STR 5L. REPAIRED ON FASI WO 20006. N/R 02027. INSTALLED REPAIR ANGLE TO FUSELAGE FRAME AT BS 380, STR 5L IAW B727 SRM 53-10-4 FIG 1, REV 102. MATERIAL USED; 7075-O, HEAT TREATED TO T-6 CONDITION. DIM.; 11 BY 1 BY 0.063.
- [SDR FOTR20006NR2023](https://openairdocs.org/sdr/FOTR20006NR2023.md): Skin · debonded · Feb 8, 2010 · N286SC · Boeing 7272A1 · Aileron Tabs
  > RT OTBD AILERON TAB, UPPER SURFACE INBD END HAS AREA OF DISBOND. REPAIRED ON FASI WO 20006. N/R 02023, INSTALLED HOT BONDED REPAIR TO RT OTBD AILERON TAB UPPER SURFACE AT INBD END IAW SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: CORE; 5052-44-3/16 DIM. 13"
- [SDR FOTR20006NR2021](https://openairdocs.org/sdr/FOTR20006NR2021.md): Skin · punctured · Feb 8, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT WING OTBD FORE FLAP HAS SEVERAL GOUGES. REPAIRED ON FASI W/0 NR 20006, N/R 02021" INSTALLED REPAIR DOUBLER TO RT WING OTBD FORE FLAP AT WS 465 IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG 1, REV 102. MATERIAL USED; 2024-T3, DIM.; 3.5" X 3.75" X 0.063".
- [SDR FOTR20006NR2020](https://openairdocs.org/sdr/FOTR20006NR2020.md): Stringer Clip · punctured · Feb 8, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Attach Fittings
  > FRAME TO STR. BRACKET HAS HOLE IN RADIUS AT STA. 672 STR. 13L. REPAIRED ON FASI W/O NR 20006, N/R 02020- R & R SUPPORT ANGLE AT STA 672 STR 13L IAW SRM 51-30-2, REV 102 AND DWG AE4899 DATED 6/29/92.
- [SDR FOTR20006NR2016](https://openairdocs.org/sdr/FOTR20006NR2016.md): Skin · gouged · Feb 8, 2010 · N286SC · Boeing 7272A1 · Leading Edge Devices
  > LT WING NR 4 SLAT OTBD END GOUGED. REPAIRED ON W/O NR 20006, N/R 02016- R & R LT WING NR4 SLAT OTBD RIB IAW SRM 51-30-2, REV 102 WITH PN 65-17286-13.
- [SDR FOTR20006NR2013](https://openairdocs.org/sdr/FOTR20006NR2013.md): Wedge · delaminated · Feb 8, 2010 · N286SC · Boeing 7272A1 · Ailerons
  > RT AILERON OTBD T/E WEDGE HAS AREA OF DISBOND ON UPPER INBD END. REPAIRED ON FASI W/O NR 20006, N/R 02013. INSTALLED HOT BONDED REPAIR TO RIGHT WING OTBD AILERON TRAILING EDGE WEDGE UPPER OTBD END IAW B727 SRM 51-40-20 PARA. 8 AND PARA 20 REV 102. MATERIAL
- [SDR FOTR20006NR2012](https://openairdocs.org/sdr/FOTR20006NR2012.md): Skin · delaminated · Feb 8, 2010 · N286SC · Boeing 7272A1 · Ailerons
  > RT OTBD AILERON T/E WEDGE HAS AREA OF DISBOND ON UPPER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 02012 - INSTALLED HOT BONDED REPAIR TO RT WING OTBD AILERON T/E WEDGE UPPER SURFACE IAW SRM 51-40-20 PARA 8 AND PARA 20 REV 102. MATERIAL USED: 2024 T3, 0.012".
- [SDR FOTR20006NR2011](https://openairdocs.org/sdr/FOTR20006NR2011.md): Skin · delaminated · Feb 8, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT WING OTBD AFT FLAP IS DELAMINATED AT STA WBL 338. REPAIRED ON FASI W/O NR 20006, N/R 2011 INSTALLED HOT BONDED REPAIR TO RT WING OTBD AFT FLAP AT WBL 228 IAW SRM 51-40-20 PARA 7 AND PARA 20 REV 102. MATERIAL USED: 7075-T7, 0.012". DIM; FILLER; 1" X 4", DOU
- [SDR FOTR20006NR1992](https://openairdocs.org/sdr/FOTR20006NR1992.md): Skin · dented · Feb 6, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT WING INBD FLAP LOWER SURFACE IS DENTED AT WS 135. REPAIRED ON FASI W/O 20006, N/R 01992, INSTALLED HOT BONDED REPAIR TO LOWER SURFACE OF RT INBD AFT FLAP AT WS 135 IAW SRM 51-40-20 PARA 7, PARA 8 AND PARA 20, REV 102. MATERIAL USED: 7075-T6, 0.016". DIM; F
- [SDR FOTR20006NR1984](https://openairdocs.org/sdr/FOTR20006NR1984.md): Stringer · corroded · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > AFT AIRSTAIR AT BS 1323 CENTER STRINGER AT LOWER END CORRODED. REPAIRED ON FSAI W/O NR 20006, N/R 01984. REPAIRED STRINGER AT AFT STAIRS STA 1323 IAW B727 SRM 53-10-3 FIG 1 AND 52-10-1 FIG 3, REV 102. MATERIAL USED: STRINGER; BAC1498-138 7075-T62, DIM: 12.0
- [SDR FOTR20006NR1976](https://openairdocs.org/sdr/FOTR20006NR1976.md): Web · cracked · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > LT SIDE OF FUSELAGE INTERIOR WEB CRACKED JUST ABOVE NR 2 ENG "S" DUCT AT BS 1303. REPAIRED ON FASI W/O NR 20006, N/R 01976. INSTALLED REPAIR DOUBLER TO CRACKED WEB ABOVE NR 2 ENGINE S DUCT AT BS 1303 IAW B727 SRM 51-40-2, FIG 1, REV 102. MATERIAL USED: DOUB
- [SDR FOTR20006NR1972](https://openairdocs.org/sdr/FOTR20006NR1972.md): Doubler · cracked · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > L1 DOOR UPPER HINGE SKIN DOUBLER CRACKED LOWER CORNER. REPAIRED ON FASI W/O NR 20006, N/R 01972. REPLACED EXTERNAL DOUBLER AT LEFT FORWARD ENTRY DOOR UPPER HINGE CUTOUT AT BS 303 IAW S/B 727-53A0198 REV. 3 DUE TO CRACK. MATERIAL USED: 3011/2 HD STAINLESS ST
- [SDR FOTR20006NR1971](https://openairdocs.org/sdr/FOTR20006NR1971.md): Shear Tie · cracked · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Internal Mounting Structure
  > STA 600 STR 16L SHEAR TIE CRACKED. REPAIRED ON FASI W/O NR 20006, NR 01971, REPLACED CRACKED SHEAR TIE AND DOUBLER AT BS 680, STR 16L IAW B727 SRM 53-20-2 FIG 3 AND 53-10-4 FIG 11, REV 102. MATERIAL USED: 7075-O, HEAT TREATED TO T6 CONDITION. DIM.; DOUBLER;
- [SDR FOTR20006NR1969](https://openairdocs.org/sdr/FOTR20006NR1969.md): Stringer Clip · cracked · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Attach Fittings
  > STA 700 STR. 16L STR CLIP CRACKED. REPAIRED ON FASI W/O NR 20006,NR 01969. REPLACED CRACKED STRINGER CLIPS AT BS 700 STR 16L IAW DRAWING NR 66-11809 REV B AND B727 SRM 51-30-2 REV 102. MATERIAL USED; 7075-T6, DIM.; 4.6 BY 3.1 BY 0.040.
- [SDR FOTR20006NR1965](https://openairdocs.org/sdr/FOTR20006NR1965.md): Frame · dented · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > STA 720A STR 16R FRAME IS DENTED. REPAIRED ON FASI W/O NR 20006, NR 01965. INSTALLED REPAIR DOUBLER TO FRAME AT BS 720A, STR 16R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1.
- [SDR FOTR20006NR1962](https://openairdocs.org/sdr/FOTR20006NR1962.md): Frame · gouged · Feb 5, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > LEFT UPPER CABIN FRAME GOUGED AT BS 670 BETWEEN STR 5L AND 6L. REPAIRED ON FASI W/O 20006, N/R 01962. REMOVED AND REPLACED FUSELAGE FRAME AT BS 670 BETWEEN STR 4L TO STR 14L WITH P/N AE2330-11 IAW AEI DRAWING AE4899 CHANGE H DATED 06/29/1992, DUE TO GOUGING.
- [SDR FOTR20006NR1862](https://openairdocs.org/sdr/FOTR20006NR1862.md): Frame · bent · Feb 4, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > STA 420 FRAME BENT AT STR 7R. REPAIRED ON FASI W/O NR 20006, NR 01862. INSTALLED REPAIR DOUBLER TO FRAME AT BS 420, STR 7R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDITION. DIM
- [SDR FOTR20006NR1850](https://openairdocs.org/sdr/FOTR20006NR1850.md): Structure · punctured · Feb 4, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT INBD AFT FLAP LOWER SURFACE IS PUNCTURED NEAR INBD END. REPAIRED ON FASI W/O NR 20006, NR 01850. INSTALLED HOT BONDED REPAIR TO RIGHT INBD AFT FLAP LOWER SURFACE AT WBL 75 IAW B727 SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: 2024-T3, 0.012 THICK, 3 DIA
- [SDR FOTR20006NR5780](https://openairdocs.org/sdr/FOTR20006NR5780.md): Web · corroded · Feb 3, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > LT MOP SILL CORRODED UNDERSIDE STA 1130 BELOW FLOOR. REPAIRED ON FASI WO 20006, N/R 05780. REMOVED AND REPLACED WEB BETWEEN STA 1110 TO 1130 IAW B727 SRM 53-10-2 FIG 5, 51-30-5, 51-30-6 AND 51-10-1, REV 102. MATERIAL USED: 7075-T6, 0.063, DIM: 18.620 BY 7.0
- [SDR FOTR20006NR5718](https://openairdocs.org/sdr/FOTR20006NR5718.md): Floorbeam · cracked · Feb 3, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Floor Beam
  > MAIN CABIN OVERWING FLOORBEAM T-CHORD CRACKED AT BS 760 RBL.45.5. REPAIRED ON FASI W/O NR 20006, N/R 05718. REMOVED AND REPLACED MAIN CABIN FLOORBEAM T-CHORD AT STA 760.9 IAW BOEING DWG 65-16279 REV A. MATERIAL USED: BAC1506-1108, DIM: 110.0 L.

Next page: https://openairdocs.org/model/boeing-727-2a1/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 aircraft_model_key = '7272A1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2a1/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.