# Service difficulty reports: Pratt & Whitney JT8D-17R

A list on [Pratt & Whitney JT8D-17R](https://openairdocs.org/engine/pratt-whitney-jt8d-17r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 102 reports

- [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 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 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 C8GA2010000080](https://openairdocs.org/sdr/C8GA2010000080.md): Duct · cracked · Dec 22, 2010 · N308AS · Boeing 727227 · Airfoil Anti/De-ice System
  > SHORTLY AFTER TAKEOFF FROM WHEN THE WING ANTI-ICE WAS TURNED ON, A LOUD POP WAS HEARD FOLLOWED BY A SPIKE IN THE ACFT PRESSURIZATION AND THE LOWER AFTER BODY HEAT LIGHT ILLUMINATED. ACFT DIVERTED AND MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. MX FOUND THE
- [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 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 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 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 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 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 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 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 FOTR20006NR1778](https://openairdocs.org/sdr/FOTR20006NR1778.md): Skin · delaminated · Feb 3, 2010 · N286SC · Boeing 7272A1 · Ailerons
  > RT OTBD AILERON T/E WEDGE PUNCTURED ON LOWER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 01778 - INSTALLED HOT BONDED REPAIR DOUBLER TO RT OTBD AILERON TAB IAW SRM 51-40-20 PARA 7, 20 AND 22, REV 102. MATERIAL USED: 2024-T3, 0.012” THICK, DIM.; 3 X 3. CALCULAT
- [SDR FOTR20006NR1794](https://openairdocs.org/sdr/FOTR20006NR1794.md): Skin · cracked · Feb 3, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT OTBD FORE FLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O 20006, NR 01794. INSTALLED REPAIR DOUBLER TO RT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-2, FIG 4 AND 57-50-4 FIG 1 REV 102. MATERIAL USED: 2024-T3, DIM.; 5 X 3 X 0.063.
- [SDR FOTR20006NR1795](https://openairdocs.org/sdr/FOTR20006NR1795.md): Skin · cracked · Feb 3, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > LT OTBD FOREFLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O NR 20006,NR 01795 - INSTALLED REPAIR DOUBLER TO LT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-4 FIG 7 REV 102. MATERIAL USED: 2024-T3, DIM.; 6 X 4 X 0.063.
- [SDR FOTR20006NR1798](https://openairdocs.org/sdr/FOTR20006NR1798.md): Intercostal · cracked · Feb 3, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > AFT PIT HAS A CRACK AT INTERCOSTAL STR 23L BETWEEN BS 950D TO 950E. REPAIRED ON FASI W/O NR20006, NR01798. R & R CRACKED INTERCOSTAL BETWEEN BS 950D TO BS 950E, STR 23L IAW SRM 51-20-1 FIG 1 REV 102 AND DWG NR 65-56125. MATERIAL USED: 7075-T6, DIM.; 19.5 X 4
- [SDR FOTR20006NR1841](https://openairdocs.org/sdr/FOTR20006NR1841.md): Frame · dented · Feb 3, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > MAIN CABIN FRAME BS.400 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/O 20006,NR 01841 INSTALLED REPAIR DOUBLER TO FRAME AT BS 400, STR 6R, DUE TO DENT, IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDI
- [SDR FOTR20006NR5629](https://openairdocs.org/sdr/FOTR20006NR5629.md): Stringer · cracked · Feb 2, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > CABIN AREA STA 720C AFT OF LIGHT HSG, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO20006. N/R 05629- REPAIRED STR 15L AT STA 720C IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: CHANNEL; 7075-T6, 0.040", DIM: 6.0" X 0.750", RADIUS FILLER; 7075-T6, 0.080", DI
- [SDR FOTR20006NR5630](https://openairdocs.org/sdr/FOTR20006NR5630.md): Stringer · cracked · Feb 2, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > CABIN AREA STA 720B FWD OF LIGHT HOUSING, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05630- REPAIRED STR 15L AT STA 720B IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: ANGLE; 7075-T6, 0.040", DIM: 6.0".
- [SDR FOTR20006NR5633](https://openairdocs.org/sdr/FOTR20006NR5633.md): Stringer Clip · cracked · Feb 2, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Attach Fittings
  > CABIN AREA STA 700, STRINGER 7L FRAME TO STRINGER BRACKET IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05633- R & R STRINGER TO FRAME CLIP AT STR 7L, STA 700 IAW DWG 65-45313 REV E AND SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032", DIM: 3.60" X 1.80".
- [SDR FOTR20006NR5665](https://openairdocs.org/sdr/FOTR20006NR5665.md): Skin · delaminated · Feb 2, 2010 · N286SC · Boeing 7272A1 · Aileron Tabs
  > LT IB AILERON TAB LOWER SURFACE OTBD HAS DELAMINATION AREA-MARKED. REPAIRED ON FASI WO 20006. N/R 05665- INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 295 IAW SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012", DIM:
- [SDR FOTR20006NR5450](https://openairdocs.org/sdr/FOTR20006NR5450.md): Frame · dented · Feb 1, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > UPPER FLANGE OF AFT PIT FRAME DENTED AT BS950F STR 25L-27L. REPAIRED ON FASI W/O 20006 REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950F BETWEEN STR 25L AND 27L IAW SRM 53-10-2 FIG. 5 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM:
- [SDR FOTR20006NR5600](https://openairdocs.org/sdr/FOTR20006NR5600.md): Frame · dented · Feb 1, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > FWD CARGO COMPT FRAME BS 680 UPPER FLANGE IS DENTED AND WEB IS BENT BETWEEN STR 23L-24L. REPAIRED ON FASI WO20006. N/R 05600- REPAIRED FRAME AT STA 680 BETWEEN STR 23L AND 24L IAW B727 SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 70
- [SDR FOTR20006NR5604](https://openairdocs.org/sdr/FOTR20006NR5604.md): Frame · dented · Feb 1, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Frame
  > FWD CARGO COPT FRAME 720A HAS 2 DENTS IN THE UPPER FLANGE BETWEEN STR 24L-25L. REPAIRED ON FASI WO20006. N/R 05604- REPAIRED FRAME AT STA 720A BETWEEN STR 24L AND 25L IAW SRM 51-30-2 AND 51-40-3 FIG. 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050", DIM: 3
- [SDR FOTR20006NR5351](https://openairdocs.org/sdr/FOTR20006NR5351.md): Skin · cracked · Jan 30, 2010 · N286SC · Boeing 7272A1 · Wing, Plate/Skin
  > NR 11 SPOILER 2ND HINGE CUTOUT IS CRACKED AT WS 460. REPAIRED ON FASI WO 20006. N/R 05351- REPAIRED NR11 SPOILER 2ND HINGE CUTOUT AT WS 460 IAW SRM 57-30-4 FIG 10, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071", DIM: 6.0" X 4.50".
- [SDR FOTR20006NR5289](https://openairdocs.org/sdr/FOTR20006NR5289.md): Skin · cracked · Jan 30, 2010 · N286SC · Boeing 7272A1 · Wing, Plate/Skin
  > LT WING, STA 549, UPPER L/E SLAT TRACK CUTOUT IS CRACKED IN UPPER RADIUS. REPAIRED ON FASI WO 20006. N/R 05289- REPAIRED LT WING UPPER L/E SLAT TRACK CUTOUT AT WS 549 IAW SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 9.50" X 10.0
- [SDR FOTR20006NR5306](https://openairdocs.org/sdr/FOTR20006NR5306.md): Hinge Bracket · cracked · Jan 30, 2010 · N286SC · Boeing 7272A1 · Spoilers
  > RT WING NR 14 SPOILER OTBD HINGE BRACKET IS CRACKED. REPAIRED ON FASI WO 2000. N/R 05306- R & R RT WING NR 14 SPOILER HINGE BRACKET IAW SRM 51-20-1 FIG 7, REV 102 AND DWG 65-21657 REV E MATERIAL USED: 7075-T6, 0.080", DIM: 4.0" X 3.0".
- [SDR FOTR20006NR5097](https://openairdocs.org/sdr/FOTR20006NR5097.md): Skin · gouged · Jan 30, 2010 · N286SC · Boeing 7272A1 · Elevator, Plate/Skin
  > RT ELEVATOR UPPER SKIN GOUGED AT ELEVATOR STA 118. REPAIRED ON FASI WO 20006, N/R 05097- REPAIRED RT ELEVATOR UPPER SKIN AT ELEV STA 118 IAW SRM 55-20-3 FIG, 4 AND 55-20-2 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.032", DIM: 7.375" X 4.125", FILLER; 2
- [SDR FOTR20006NR5267](https://openairdocs.org/sdr/FOTR20006NR5267.md): Skin · punctured · Jan 30, 2010 · N286SC · Boeing 7272A1 · Elevator, Plate/Skin
  > (FOTR) RT ELEVATOR UPPER SKIN PUNCTURED AT ELEV STA 67. REPAIRED ON FASI W/O NR 20006, 05267- REPAIRED RT ELEVATOR UPPER SKIN AT ELEV STA 67 IAW SRM 55-20-3 FIG, 4 AND 55-20-2 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.032", DIM: 4.625" X 4.125". CU
- [SDR FOTR20006NR5160](https://openairdocs.org/sdr/FOTR20006NR5160.md): Skin · debonded · Jan 29, 2010 · N286SC · Boeing 7272A1 · Spoilers
  > NR 6 SPOILER PANEL LOWER IB SKIN DOUBLER & HINGE FITTING IS DISBONDED. REPAIRED ON FASI WO 20006. N/R 05307- INSTALLED BONDED REPAIR DOUBLER TO RT WING NR 9 SPOILER T/E AT WBL 130.0 IAW SRM 51-40-20, REV 102. MATERIAL USED: FILLER; 7075-T6, 0.020", DIM: 2.0"
- [SDR FOTR20006NR5184](https://openairdocs.org/sdr/FOTR20006NR5184.md): Skin · chafed · Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > LT OB FORE FLAP UPPER OB LE WBL 485 HAS A DEEP CHAFED AREA ON THE REPAIR DOUBLER. REPAIRED ON FASI WO 20006. N/R 05184- R & R PREVIOUS DOUBLER AT LT WING OTBD FORE FLAP OTBD L/E AT WBL 485.0 IAW SRM 57-50-4 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.0
- [SDR FOTR20006NR5171](https://openairdocs.org/sdr/FOTR20006NR5171.md): Skin · dented · Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > LT INBD AFT FLAP INBD LOWER SURFACE HAS 2 LARGE SHALLOW DENTS. REPAIRED ON FASI WO 20006. N/R 05171- REPAIRED LT WING INBD AFT FLAP LOWER SURFACE AT WBL 86.0 BY HOT BONDING REPAIR IAW SRM 51-40-20, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.020", DIM: 11.50
- [SDR FOTR20006NR5222](https://openairdocs.org/sdr/FOTR20006NR5222.md): Spar · damaged · Jan 29, 2010 · N286SC · Boeing 7272A1 · Elevator, Spar/Rib
  > C/W AD2008-17-14 SB 727-55-0089 ELEVATOR REAR SPAR AT THE TAB HINGE LOC. IAW PARA (A) REPLACEMENT OF THE ELEVATOR REAR SPAR AND SUPPORT FITTING IAW PART 2 OF S/B 727-55-0089 REV 1 (RT). REPAIRED ON FASI WO 20006. N/R 05222- R & R ELEVATOR REAR SPAR AND SUPP
- [SDR FOTR20006NR5050](https://openairdocs.org/sdr/FOTR20006NR5050.md): Skin · damaged · Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT WING AFT IB FLAP LOWER SURFACE HAS GRAVEL DAMAGE AT INBD END. REPAIRED ON FASI WO 20006. N/R 05050- REPAIRED RT WING AFT INBD FLAP LOWER SURFACE AT WBL 115.0 BY HOT BONDING REPAIR IAW SRM 51-40-20 AND 57-50-2 FIG 3, REV 102. MATERIAL USED: DOUBLER- 7075-T6
- [SDR FOTR20006NR5049](https://openairdocs.org/sdr/FOTR20006NR5049.md): Skin · gouged · Jan 29, 2010 · N286SC · Boeing 7272A1 · Trailing Edge Flaps
  > RT WING INBD FORE FLAP OB LOWER SKIN IS GOUGED. REPAIRED ON FASI WO 20006. N/R 05049- REPAIRED RT WING INBD FORE FLAP OTBD LOWER SKIN AT STA 240.0 IAW SRM 57-50-4 FIG 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 5.250" X 4.125".
- [SDR FOTR20006NR5044](https://openairdocs.org/sdr/FOTR20006NR5044.md): Skin · delaminated · Jan 29, 2010 · N286SC · Boeing 7272A1 · Ailerons
  > RT WING AILERON OTBD T/E WEDGE IS DELAMINATED AT OTBD END. REPAIRED ON FASI WO 20006. N/R 05044- REPAIRED RT WING OTBD T/E WEDGE BY HOT BONDING REPAIR IAW SRM 51-40-20, REV 102, CUT OUT, AND FILLER DIM: 1.0" X 1.0", 3.0" X 1.0", AND 4.0" X 1.0". MATERIAL US
- [SDR FOTR20006NR5029](https://openairdocs.org/sdr/FOTR20006NR5029.md): Skin · cracked · Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge Devices
  > RT WING NR 8 SLAT TE HAS 2 CRACKS COMING FROM SCREW HOLE SLAT STA 407.5. REPAIRED ON FASI WO 20006. N/R 05029- INSTALLED DOUBLER REPAIR TO RT WING NR 8 SLAT T/E AT SLAT STA 407.5 IAW SRM 57-50-3 FIG 10, REV 102 MATERIAL USED: DOUBLER- 7075-T6’ 0.125", DIM: 8.
- [SDR FOTR20006NR4982](https://openairdocs.org/sdr/FOTR20006NR4982.md): Skin · cracked · Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge Devices
  > RT WING NR 6 SLAT LOWER SKIN COMMON TO TRACK IS CRACKED IN 2 PLACES SLAT SLAT STA 216. REPAIRED ON FASI WO 20006. N/R 04982- INSTALLED DOUBLER REPAIR TO RT WING NR 6 SLAT LOWER SKIN AT SLAT STA 216.0 IAW SRM 57-50-3 FIG 1, REV 102. MATERIAL USED: 2024-T3, 0.
- [SDR FOTR20006NR4981](https://openairdocs.org/sdr/FOTR20006NR4981.md): Skin · cracked · Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge Devices
  > RT WING FIXED L/E NR 6 SLAT OTBD HOOK SEAL CUTOUT AFT SIDE IS CRACKED. REPAIRED ON FASI WO 20006. N/R 04981- REPAIRED RT WING FIXED L/E AT NR 6 SLAT OTBD HOOK SEAL CUT-OUT AFT SIDE AT STA 530.0 IAW SRM 57-30-4 FIG. 9 AND 51-10-1, REV 102. CUT- OUT DIM: 8.50"
- [SDR FOTR20006NR4980](https://openairdocs.org/sdr/FOTR20006NR4980.md): Skin · torn · Jan 29, 2010 · N286SC · Boeing 7272A1 · Leading Edge Devices
  > RT WING FIXED L/E NR 6 SLAT INBD HOOK SEAL CUTOUT AFT SIDE HAS 2 MISSING FASTENERS. REPAIRED ON FASI WO 2000654. N/R 04980- REPAIRED RT WING FIXED L/E AT NR 6 SLAT INBD HOOK SEAL CUTOUT AFT SIDE AT STA 519 IAW SRM 57-30-4 FIG 9, REV 102. MATERIAL USED: DOU
- [SDR FOTR20006NR4642](https://openairdocs.org/sdr/FOTR20006NR4642.md): Skin · dented · Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > (FOTR) DENT ON RT FUSELAGE SKIN AT BS 1100 ABOVE STR 19R. REPAIRED ON FASI WO 20006. N/R 04642 INSTALLED REPAIR DOUBLER AT BS 1100 ABOVE STR 19R, IAW SRM 53-30-3 FIG 3, REV 102 MATERIAL USED: 2024-T3 DIM. 12.25" X 9" X 0.071".
- [SDR FOTR20006NR4685](https://openairdocs.org/sdr/FOTR20006NR4685.md): Hinge · cracked · Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage, Door Hinge
  > EXT FUSELAGE MCD AFT MOST SEGMENT FUSELAGE SIDE HAS 2ND AFT LOBE CRACKED. REPAIRED ON FASI WO 20006. R & R MAIN CARGO DOOR AFT HINGE SECTION WITH PN MS20001-16-7200 AT STA 620 IAW B727 FREIGHTER MM, CH 52, FIG 5201B, REV. G.
- [SDR FOTR20006NR4709](https://openairdocs.org/sdr/FOTR20006NR4709.md): Stiffener · corroded · Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > (FOTR) CORROSION AT 227.8 BULKHEAD, BL 0 SKIN INTERIOR, JUST AFT OF EQUIPMENT BAY ACCESS DOOR. REPAIRED ON FASI WO 20006. N/R 04709- R & R DAMAGED STIFFENER AT BL 0 STA 227.8 IAW SRM 51-30-2, 53-10-1 FIG. 1, REV 102 AND DWG 69-15768. MATERIAL USED: 7075-T6,
- [SDR FOTR20006NR4715](https://openairdocs.org/sdr/FOTR20006NR4715.md): Skin · dented · Jan 27, 2010 · N286SC · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > (FOTR) DENT AT L FUSELAGE SKIN AT BS 356 BELOW STR 24L. REPAIRED ON FASI WO 20006. REPAIRED LT FUSELAGE SKIN AT STA 356.0 BETWEEN STR 24L AND 25L IAW DWG AJ07-53-102 REV. IR. 8110-3 DATED 02/12/2010 ISSUED. REWORKED LOWER SKIN LAP SEAM AND CUT OUT DAMAGED SECT
- [SDR DHLA200800094](https://openairdocs.org/sdr/DHLA200800094.md): Nose Bullet · contaminated · Aug 29, 2008 · N741DH · Boeing 7272Q9 · Turbine Engine Air Inlet Section
  > WHEN TAKE OFF THRUST WAS APPLIED ENG NR 1 AND NR 3 AT 2.19 EPR SHOWED 88% N1 520* EGT. 90% N2. FAILED TO MAKE TAKE OFF OFF THRUST. REMOVED DEBRIS WITH DRY NITROGEN OUTWARD THROUGH NOSE DOME ON NR 1 & NR 3 ENG. NOSE DOME NOT REMOVED. PT 2 LINES RESECURED.
- [SDR DHLA200800080](https://openairdocs.org/sdr/DHLA200800080.md): Transmitter · malfunctioned · Jul 17, 2008 · N741DH · Boeing 727200 · Engine Pressure Ratio (EPR)
  > FLT 577, DURING ENG ACCELERATION NR 3 EPR FLUCTUATES RAPIDLY. ALL OTHER ENG PARAMETERS NORMAL. BRAKE ENERGY NORMAL. DEFERRED PER MEL 77-1-1, DMI CONTROL 3319. MAINTENANCE CONTROLLER RPR AT 0942(Z). AIRCRAFT GROUNDED. REMOVED AND REPLACED NR 3 ENG EPR TRA
- [SDR C8G2008F00000](https://openairdocs.org/sdr/C8G2008F00000.md): Engine · locked · Jun 3, 2008 · N89427 · Boeing 727227 · Engine (Turbine/Turboprop)
  > DURING APPROACH, THE NR 3 ENGINE COMPRESSOR STALLED AND ENGINE FLAMED OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 WAS UN-MOVEABLE. REMOVED AND REPLACED NR 3 ENGINE, OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS WERE NOTED. A
- [SDR C8GA20080016](https://openairdocs.org/sdr/C8GA20080016.md): Compressor · stalled · Jun 3, 2008 · N89427 · Boeing 727227 · Turbine Engine Compressor Section
  > FLT 0001 FROM MIA-PTY. DURING APPROACH TO PTY THE NR 3 ENG COMPRESSOR STALLED AND ENG FLAMED OUT. THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 UNMOVEABLE. REMOVED AND REPLACED THE NR 3 ENGINE. OPS AND LEAK CHECKS GOOD. NO OTHER D
- [SDR I5PA2008001](https://openairdocs.org/sdr/I5PA2008001.md): Line · broken · Mar 7, 2008 · N86425 · Boeing 727212 · Turbine Engine Oil System
  > AT FLIGHT LEVEL 30K FEET 263 NM OUT OF MAJURO, NR 1 OIL QUANTITY STARTED TO DECREASE FROM 4 GALLONS TO ZERO, CREW THEN SHUT DOWN ENGINE AND DESCENDED TO FL 26K FEET, RETURNED TO MAJURO. WINDMILLING OCCURRED FOR 43 MINUTES WITH OIL PRESSURE AT 17-18 PSI. ON I
- [SDR C7WA200700001](https://openairdocs.org/sdr/C7WA200700001.md): Controller · smoke · Apr 29, 2007 · N1279E · Boeing 7272Q6 · Cargo/Baggage Doors
  > ON CLIMBOUT FROM SJU FLIGHT ENGINEER SMELLED SMOKE AND TRIED TO ID SOURCE. ACCOMPLISHED AOM PROCEDURE AND REMOVED POWER FROM CARGO DOOR CONTROL. SMOKE STOPPED AND RETURNED FOR INSPECTION. [06-21-07] INSPECTION OF CARGO DOOR CONTROL AREA REVEALED THE HYDR

Next page: https://openairdocs.org/engine/pratt-whitney-jt8d-17r/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 engine_model_key = 'JT8D17R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt8d-17r/reports

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