# Service difficulty reports: Pratt & Whitney JT8D-217A

A list on [Pratt & Whitney JT8D-217A](https://openairdocs.org/engine/pratt-whitney-jt8d-217a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 235 reports

- [SDR AALA20170321006](https://openairdocs.org/sdr/AALA20170321006.md): Bolt · worn · Mar 21, 2017 · N434AA · Doug MD83 · Engine Anti-Icing System
  > FLIGHT DIVERTED DUE TO AN AIRFRAME VIBRATIONS BETWEEN THE AFT LAVATORIES. UNEVENTFUL LANDING. LEFT ENGINE ANTI-ICE VALVE MOUNTING BOLT WORN AND LOOSE. REMOVED AND REPLACED WITH NEW HARDWARE IAW AMM 75-10-01. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
- [SDR AALA20150612001](https://openairdocs.org/sdr/AALA20150612001.md): Compressor Blade · damaged · Jun 11, 2015 · N955U · Doug DC982 · Turbine Engine Compressor Section
  > AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CREW REPORTS A COMPRESSOR STALL ON RT ENG FOLLOWED BY A REDUCTION IN EPR & INCREASE IN EGT. ACCOMPLISHED CARD 72-96-12 71-91-12 & BORESCOPE WITH A DETAILED VISU
- [SDR AALA20110331TUL07](https://openairdocs.org/sdr/AALA20110331TUL07.md): Exciter · failed · Mar 31, 2011 · N436AA · Doug DC983 · Exciter
  > MCO INFLIGHT TPA-ORD. CREW REPORTED LIGHTNING STRIKE TO RIGHT SIDE OF AIRCRAFT WITH RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 1 MINUTE). EMERGENCY DECLARED DIVERTED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE EXCITER,
- [SDR AALA20100418SFO01](https://openairdocs.org/sdr/AALA20100418SFO01.md): Tube · leaking · Apr 18, 2010 · N433AA · Doug DC983 · Turbine Engine Oil System
  > SFO - CREW REPORTED RIGHT ENGINE OIL PRESSURE LIGHT DROPPED TO 20 PSI AND STABILIZED. RIGHT HAND THROTTLE REDUCED TO IDLE. FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. FOUND OIL LEAK AT 11 O`CLOCK POSITION. REMOVED AND REPLACED OIL TUBE AT OIL FILTER DIFFE
- [SDR ASMF200711003](https://openairdocs.org/sdr/ASMF200711003.md): Blade · damaged · Nov 12, 2007 · N501AM · Doug DC982 · Turbine Engine Compressor Section
  > DURING TRANSIT CHECK, FIVE BLADES WERE DETECTED DAMAGED DUE TO A FOD IN LT ENGINE. (4) BLADES WERE DETECTED WITH NICKS ON BLADES LEADING EDGE AND WERE REWORKED IAW MM 72-33-21 BEING WITHIN LIMITS. ONE BLADE WAS DETECTED WITH DENT WITH DEPTH OF 0.135 INCHES AND
- [SDR ASMF200708007](https://openairdocs.org/sdr/ASMF200708007.md): Control Valve · leaking · Aug 25, 2007 · N501AM · Doug DC821 · Engine Thrust Reverser
  > DURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LT ENGINE REVERSE CONTROL VALVE. THE VALVE WAS REPLACED IAW MM 78-31-04, TESTED CORRECT AND 6/4 OF HYDRAULIC FLUID WERE REPLENISHED IAW MM 12-13-82.
- [SDR GTIA200700015](https://openairdocs.org/sdr/GTIA200700015.md): Floorbeam · corroded · Feb 17, 2007 · N804NK · Doug DC982 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CORRODED. REPLACED FLOOR SUPPORT BEAM.
- [SDR GTIA200700013](https://openairdocs.org/sdr/GTIA200700013.md): Intercostal · cracked · Feb 16, 2007 · N804NK · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT CARGO CABIN FLOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL.
- [SDR GTIA200700014](https://openairdocs.org/sdr/GTIA200700014.md): Floorbeam · corroded · Feb 16, 2007 · N804NK · Doug DC982 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM ANGLE. REPLACED FLOORBEAM.
- [SDR GTIA200700012](https://openairdocs.org/sdr/GTIA200700012.md): Floorbeam · corroded · Feb 15, 2007 · N804NK · Doug DC982 · Fuselage Main, Floor Beam
  > CORROSION AFT CARGO CABIN FLOORBEAM. INSTALLED NEW FLOORBEAM.
- [SDR GTIA200700009](https://openairdocs.org/sdr/GTIA200700009.md): Floor Support · corroded · Feb 14, 2007 · N804NK · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT. REPAIRED FLOOR SUPPORT.
- [SDR GTIA200700010](https://openairdocs.org/sdr/GTIA200700010.md): Floorbeam · corroded · Feb 14, 2007 · N804NK · Doug DC982 · Fuselage Main, Floor Beam
  > CORROSION AT FWD CABIN FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT.
- [SDR GTIA200700011](https://openairdocs.org/sdr/GTIA200700011.md): Floorbeam · corroded · Feb 14, 2007 · N804NK · Doug DC982 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM. INSTALLED NEW FLOORBEAM.
- [SDR GTIA200700008](https://openairdocs.org/sdr/GTIA200700008.md): Longeron · corroded · Feb 12, 2007 · N804NK · Doug DC982 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT LONGERON 29R HAS CORROSION. MADE LONGERON REPAIR.
- [SDR GTIA200700007](https://openairdocs.org/sdr/GTIA200700007.md): Door · obstructed · Feb 10, 2007 · N804NK · Doug MD83 · Emergency Exits
  > UNABLE TO OPEN RT AFT OVERWING EXIT. FOUND TRIM PANEL OVERLAPPING UPPER AFT CORNER PREVENTING IT FROM OPENING.
- [SDR ASMF200612002](https://openairdocs.org/sdr/ASMF200612002.md): Regulator Valve · failed · Dec 11, 2006 · N501AM · Doug DC982 · Cabin Cooling System
  > AIRCRAFT RETURNED DUE TO AIR CONDITIONING SYSTEMS FAILED, RT SYSTEM WAS SHUTDOWN, LT SYSTEM DID NOT OPERATE AND SMOKE ODOR WAS DETECTED. DURING MAINTENANCE CHECK, THE CHIP DETECTORS WERE CHECKED, WATER SEPARATORS WERE REPLACED IAW MM 21-20-2, BITE TO BOTH CONT
- [SDR ASMF200604013](https://openairdocs.org/sdr/ASMF200604013.md): Fan Blade · damaged · Apr 25, 2006 · N1003Y · Doug DC982 · Turbine Engine Compressor Section
  > DURING TRANSIT CHECK, IT WAS DETECTED ONE LEFT ENGINE C1 FAN BLADE DAMAGED BY AN SCREW SANK INTO THE ACOUSTIC PANEL (FOD). THE DAMAGE WAS EVALUATED IAW M/M 72-00-00 BEING WITHIN LIMITS. DURING OVERNIGHT CHECK, THE FAN BLADE WAS REWORKED IAW M/M 72-00-00 REMA
- [SDR ASMF200603005](https://openairdocs.org/sdr/ASMF200603005.md): Filter · dirty · Mar 13, 2006 · N501AM · Doug DC982 · Engine Fuel and Control
  > CAPTAIN REPORTED THAT DURING TAXING LT ENGINE DID NOT ACCELERATE EVEN WITH THRUST LEVER FULLY FORWARDED, RETURNING TO PLATFORM. DURING CHECK, MAINTENANCE PERSONNEL DETECTED THAT THE LT ENGINE ACCELERATED VERY SLOWLY, SO THRUST BUMP PROCEDURE WAS PERFORMED WITH
- [SDR AALA20060143](https://openairdocs.org/sdr/AALA20060143.md): Engine · shutdown · Mar 4, 2006 · N950U · Doug DC982 · Engine (Turbine/Turboprop)
  > DEN - RIGHT ENGINE FAILED AFTER TAKEOFF AT ABOUT 300 FEET ABOVE GROUND LEVEL. RIGHT HAND ENGINE EXHAUST GAS TEMPERATURE AT ROTATION WAS ABOUT 570 DEGREES. ENGINE FIRE/DAMAGE/SEPARATION CHECKLIST FOLLOWED, HAD N1 AND N2 BUT NO RESTART. LANDED DEN WITHOUT INCI
- [SDR 06FDEA0547](https://openairdocs.org/sdr/06FDEA0547.md): Fuel Control · malfunctioned · Feb 6, 2006 · N216FE · Boeing 7272S2F · Fuel Control/Turbine Engines
  > NO THROTTLE RESPONSE ON NR 1 ENGINE ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL IAW FX B 727-200 MM 73-20-001-2. PERFORMED ENGINE RUN AND TRIM MED IAW FX B727-200 MM 71-00-030 AND 71-00-097 AND OPS AND LEAK CHECK GOOD. ALSO REMOVED AND REPLACE
- [SDR ASMF200602001](https://openairdocs.org/sdr/ASMF200602001.md): Fan Blade · damaged · Feb 2, 2006 · N501AM · Doug DC982 · Turbine Engine Compressor Section
  > DURING TRANSIT CHECK, DETECTED 09 LEFT ENGINE FAN BLADES WITH DAMAGES. ONE OF THEM WAS OUT OF LIMITS. 04 FAN BLADES WERE REPLACED IAW M/M 72-33-21 AND 06 WERE REWORKED IAW M/M 72-33-22. ENGINE WAS OPERATIONAL CHECKED IAW MPCM 71-00-01 AND M/M 71-00-00, TEST
- [SDR ASMF200512019](https://openairdocs.org/sdr/ASMF200512019.md): Annunciator · failed · Dec 25, 2005 · N501AM · Doug DC982 · Leading Edge Slat Position Indicating System
  > AIRCRAFT RETURNED TO PLATFORM DURING TAXING THE SLAT DISAGREE LIGHT NOT TURNED ON. DURING MAINTENANCE REVISION, THE SLAT DISAGREE LIGHT WAS FAILING INTERMITTENTLY. THE PSEU BITE WAS PERFORMED, THE SLATS SENSORS A, B, C, D WERE CLEANED, THE COCKPIT DISAGREE LIG
- [SDR ASMF200501201](https://openairdocs.org/sdr/ASMF200501201.md): Engine · vibration · Dec 22, 2005 · N1003Y · Doug DC982 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGINE WAS SHUTDOWN, VIBRATION WAS FELT IN ALL THE AIRCRAFT. THE LT ENGINE CHIP DETECTORS, ACCESSORIES, P
- [SDR ASMF200512007](https://openairdocs.org/sdr/ASMF200512007.md): Pin · broken · Dec 7, 2005 · N1003Y · Doug DC982 · Nose/Tail Landing Gear
  > DURING PUSH BACK THE NOSE LANDING GEAR TOWING FUSE PIN WAS BROKEN. IT WAS REPLACED IAW MM 32-21-14 AND THE NOSE LANDING GEAR AND GENERAL INSPECTIONS FOR EXCESSIVE LOAD WERE PERFORMED IAW MM 05-51-03 AND MM 32-20-00 RESPECTIVELY, NO DAMAGES WERE FOUND.
- [SDR GTIA050264](https://openairdocs.org/sdr/GTIA050264.md): Frame · cracked · Oct 17, 2005 · N804NK · Doug DC982 · Fuselage Main, Frame
  > FRAME CANT 1463 AT APPROX LONGERON 19 AND 20 ON AC RT HAS CRACKED WEBBING. INSTALLED PERMANENT REPAIR ON CANTED FRAME FS 1463 BETWEEN R18L AND R25L, IAW EA REV ORIGINAL HAS BEEN ACCOMPLISHED. (K)
- [SDR ASMF200505030](https://openairdocs.org/sdr/ASMF200505030.md): Skin · cracked · May 30, 2005 · N501AM · Doug DC982 · Drag Control System
  > CAPTAIN REPORTED THAT HE PERFORMED THE FINAL APPROACH AND LANDING WITH 3450 POUNDS OUT OF BALANCE BETWEEN TANKS. OUT OF BALANCE INSPECTION WAS PERFORMED IAW MM, DETECTING A CRACK IN THE RT WING IB FLIGHT SPOILER OF 9 INCHES LONG. SPOILER WAS REPLACED IAW MM 27
- [SDR T48R20050011](https://openairdocs.org/sdr/T48R20050011.md): Engine · damaged · Apr 26, 2005 · N803NK · Doug DC982 · Engine (Turbine/Turboprop)
  > ENGINE WAS REMOVED FROM N803NK FOR INFLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED THE HPC, HPT AND LPT MODULES HAVE HEAVY IMPACT DAMAGE.
- [SDR GTIA050099](https://openairdocs.org/sdr/GTIA050099.md): Web · punctured · Apr 4, 2005 · N821NK · Doug DC982 · Fuselage Miscellaneous Structure
  > AT STA 200, NR 1 SEAT TRACK LT FLOOR WEB HAS A PUNCTURE. CUT OUT PUNCTURE FROM FLOOR WEB STA 200, NR 1 SEAT TRACK. FABRICATE DOUBLERS AND FILLERS. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER IAW SRM. (K)
- [SDR GTIA050076](https://openairdocs.org/sdr/GTIA050076.md): Wire · broken · Mar 26, 2005 · N808NK · Doug DC983 · Flight Control System Wiring
  > UPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 1485, REPAIRED BROKEN WIRE IAW SRM. OPS CHECK, OK. (K)
- [SDR GTIA050097](https://openairdocs.org/sdr/GTIA050097.md): Support Angle · cracked · Mar 25, 2005 · N821NK · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD UPLOCK SUPPORT ANGLE CRACKED. REMOVED AND FABRICATED NEW ANGLE IAW SRM. TREATED AND PRIMED, INSTALLED SUPPORT ANGLE IAW SRM. (K)
- [SDR GTIA050084](https://openairdocs.org/sdr/GTIA050084.md): Web · corroded · Mar 15, 2005 · N821NK · Doug DC982 · Fuselage Miscellaneous Structure
  > CABIN STA 180-200, RBL 54, RBL59, SUB FLOOR CORRODED. REMOVED CORROSION AT WEB. MATERIAL LOSS OUT OF LIMITS. REMOVED FWD AIRSTAIR. REMOVED FLOOR SUPPORT RT STA 160 TO 200. CUT OUT DAMAGED AREA AND FABED DOUBLER. PRIMED AND TREATED, INSTALLED FLOOR SUPPOR
- [SDR GTIA050093](https://openairdocs.org/sdr/GTIA050093.md): Strap · corroded · Mar 11, 2005 · N821NK · Doug DC982 · Fuselage Miscellaneous Structure
  > ALUMINUM STRAP ON LOWER SIDE OF L2 DOOR THRESHOLD HAS CORROSION. STRAP CORROSION IS OUT OF LIMITS. FABRICATED NEW STRAP IAW SRM. TREATED AND PRIMED, INSTALLED STRAP ON L2 DOOR THRESHOLD IAW SRM. (K)
- [SDR GTIA050079](https://openairdocs.org/sdr/GTIA050079.md): Doubler · corroded · Mar 11, 2005 · N821NK · Doug DC982 · Buffet/Galleys
  > G-2 GALLEY, CART ENCLOSURE, AFT LOWER LIP AND (2 EA) DOUBLERS ARE CORRODED. REMOVED LOWER LIP AND DOUBLERS, FOUND LIP AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS. TREAT AND PRIMED. INS
- [SDR GTIA050078](https://openairdocs.org/sdr/GTIA050078.md): Support Angle · corroded · Mar 11, 2005 · N821NK · Doug DC982 · Buffet/Galleys
  > G-2 GALLEY, UPPER SECTION, LOWER EDGE AND SUPPORT ANGLE ARE CORRODED. REMOVED CORROSION ON LOWER EDGE AND SUPPORT ANGLE. FOUND SUPPORT ANGLE OUT OF LIMITS FABRICATED SUPPORT ANGLE IAW SRM. PRIMED AND INSTALLED SUPPORT ANGLE. (K)
- [SDR GTIA050098](https://openairdocs.org/sdr/GTIA050098.md): Doubler · cracked · Mar 10, 2005 · N821NK · Doug DC982 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STABILIZER, RT SIDE IB UPPER BRACKET SUPPORT HAS CRACK ON DOUBLER. REMOVED CRACKED DOUBLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM. (K)
- [SDR GTIA050096](https://openairdocs.org/sdr/GTIA050096.md): Skin · dented · Mar 10, 2005 · N821NK · Doug DC982 · Cargo/Baggage Doors
  > DENT ON AFT CARGO DOOR SKIN 21 INCHES FROM AFT EDGE AND 11 INCHES FROM BOTTOM EDGE OF DOOR (X=0.035 INCH, D=1.75 INCH, D/X=50). STRIPPED AREA OF DENT ON AFT CARGO DOOR FS 1185 IS UNDER CONDITION IAW SRM. DYE PENETRANT INSP, NO CRACK FOUND. REMOVED LATCH HAN
- [SDR GTIA050095](https://openairdocs.org/sdr/GTIA050095.md): Skin · dented · Mar 10, 2005 · N821NK · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN FS421 BETWEEN LONGERONS 19R AND 20R (D=0.5 INCH, X=0.008 INCH, D/X - 62.5 INCHES). REMOVED CARGO DOOR TO FOM IAW SRM. FOUND DENT HAS GOUGED IN CENTER, REMOVED DAMAGED AREA OF SKIN (1.5 INCH X 0.8 INCH) IAW SRM. FABRICATED DOUBLER AND F
- [SDR GTIA050082](https://openairdocs.org/sdr/GTIA050082.md): Cusp Web · corroded · Mar 10, 2005 · N821NK · Doug DC982 · Fuselage Miscellaneous Structure
  > MID PIT STA 522-636, A LONG 18, RBL 52, FLOOR PANEL UNDER FEDDER CABLES CORRODED. REMOVED CORROSION FROM 522-636, FOUND OUT OF LIMITS. REMOVED WEB STA 503-598, FABED NEW WEB, PRIMED AND TREATED. INSTALLED WEB AT STA 503-598, RBL 52, IAW SRM. (K)
- [SDR GTIA050081](https://openairdocs.org/sdr/GTIA050081.md): Seat Track · cracked · Mar 10, 2005 · N821NK · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > RT OB SEAT TRACK HAS AREA OF CORROSION AT FS 229. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK. FOUND WEB OB OF SEAT TRACK FS 218 CRACKED, FABED DOUBLER AND FILLER IAW SRM. PRIMED AND TREATED. INSTALLED DOUBLER, FILLER AND SEAT TRACK
- [SDR GTIA050094](https://openairdocs.org/sdr/GTIA050094.md): Frame · cracked · Mar 7, 2005 · N821NK · Doug DC982 · Wing, Rib/Bulkhead
  > FROM C/O 0155770 RT WING L/E 2 EA FORMERS ST APPROX STA 351 CRACKED. FABRICATED DOUBLER IAW SRM. HEAT TREATED 2 EA DOUBLER IAW SRM. TREATED AND PRIMED INSTALLED REPAIR DOUBLER IAW SRM. LP NR 01476783. (K)
- [SDR GTIA050083](https://openairdocs.org/sdr/GTIA050083.md): Floor Support · corroded · Mar 4, 2005 · N821NK · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, STA 1174, LBL 12, MAIN CABIN FLOORBEAM UPPER FLOOR SUPPORT ANGLE IS CORRODED (EXFOLIATION). REMOVED DAMAGED FLOORBEAM AND FOUND OUT OF LIMITS. FABRICATED NEW SUPPORT ANGLE, PRIMED AND TREATED. INSTALLED FLOOR SUPPORT ANGLE IAW SRM. (
- [SDR ASMF200503002](https://openairdocs.org/sdr/ASMF200503002.md): Fuel Control · failed · Mar 3, 2005 · N501AM · Doug DC821 · Fuel Control/Turbine Engines
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE WITHOUT ACCELERATION AND PARAMETERS WERE BELOW NORMAL IN IDLE. THE ACCELERATION CHAMBER WAS SERVICED AND FCU WAS LUBRICATED IAW MM 73-00-00, TESTED CORRECT. AIRCRAFT RETURNED TO PLATFORM AGAIN DU
- [SDR GTIA050071](https://openairdocs.org/sdr/GTIA050071.md): Skin · dented · Mar 3, 2005 · N804NK · Doug DC982 · Fuselage Main, Plate/Skin
  > SKIN DENT AT STA 1174, BETWEEN LONGERON 17L AND 18L. REMOVED SAF-T-GLO, GALLEY 4 AND SIDE WALL PANEL TO FOM AT LT FS 1184. FOUND DENT TO BE (D=1.5 INCH, X=0.050, D/X=30) COND 2. REFORMED DENT AREA TO ORIGINAL CONTOUR. INSTALLED DOUBLER IAW SRM 53-04, FIG
- [SDR GTIA050055](https://openairdocs.org/sdr/GTIA050055.md): Skin · dented · Feb 27, 2005 · N804NK · Doug DC982 · Trailing Edge Flaps
  > LT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K)
- [SDR GTIA050061](https://openairdocs.org/sdr/GTIA050061.md): Floor Support · broken · Feb 26, 2005 · N804NK · Doug DC982 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STA 1136 BROKEN AFT PIT 28R-28L. REMOVED FLOOR SUPPORT AND LOCATED NEW FLOOR SUPPORT AT STA 1136, 28R-28L. INSTALLED FLOOR SUPPORT FS 1136, 28R-28L, AFT PIT IAW SRM. (K)
- [SDR GTIA050037](https://openairdocs.org/sdr/GTIA050037.md): Motor · inoperative · Feb 23, 2005 · N808NK · Doug DC983 · Flight Control System
  > PRIMARY LONG TRIM INOPERATIVE, TAIL SWAP WITH AIRCRAFT 829. REMOVED AND REPLACED LONG TRIM MOTOR AND REPAIRED MOTOR GROUNDS, SYSTEM OPS CHECK GOOD. (K)
- [SDR GTIA050056](https://openairdocs.org/sdr/GTIA050056.md): Support Angle · corroded · Feb 20, 2005 · N804NK · Doug DC982 · Fuselage Miscellaneous Structure
  > THRESHOLD SUPPORT ANGLE, STA 1212, ON DOOR JAMB BEAM IS CORRODED. REMOVED CORROSION AT SUPPORT ANGLE. MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT ANGLE AT STA 1212. FABRICATED NEW SUPPORT ANGLE, HEAT TREATED REPAIR PART. INSTALLED SUPPORT ANGLE AT STA 12
- [SDR GTIA050064](https://openairdocs.org/sdr/GTIA050064.md): Skin · dented · Feb 20, 2005 · N804NK · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT FS 304 BETWEEN LONGERON 28L-29L. (D=0.5 INCH, X=0.015 INCH D/X= 33.3). DENT WAS FOUND TO BE LESS THAN 1.0 INCH FROM FRAME REQ A CUT OUT REPAIR. CUT OUT DAMAGED SKIN AT FS 304 BETWEEN LONGERON 28L-29L. FABED NEW SKIN SECTION, REPAIR
- [SDR GTIA050053](https://openairdocs.org/sdr/GTIA050053.md): Skin · dented · Feb 19, 2005 · N804NK · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT AT FS 245, LONGERON 18L (D=1.250 INCH, X=0.054 D/X=23.14). REMOVED AIRCRAFT SKIN AT STA FS 245, LONGERON 18L (20 INCHES X 14 INCHES). FABRICATED REPAIR PARTS IAW SRM. INSTALLED, REPAIR AT FS STA 245 LONGERON 18L. (K)
- [SDR GTIA050052](https://openairdocs.org/sdr/GTIA050052.md): Stiffener · corroded · Feb 18, 2005 · N804NK · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, STA 1338, 27L-27R AFT SIDE OF FALSE BULKHEAD, LOWER STIFFENERS ARE CORRODED. REMOVED CORROSION AT STIFFENER STA 1338L, 29L. MATERIAL LOSS OUT OF LIMITS. REMOVED STIFFENER AT STA 1338L, 29L, LOCATED AND DRILLED NEW STIFFENER. INSTALLE

Next page: https://openairdocs.org/engine/pratt-whitney-jt8d-217a/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 = 'JT8D217A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt8d-217a/reports

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