# Service difficulty reports: N302FE, cancelled Feb 3, 2024

A list on [N302FE, cancelled Feb 3, 2024](https://openairdocs.org/deregistered/N302FE-2024-02-03.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 5 · 204 reports

- [SDR FDEA201411023449](https://openairdocs.org/sdr/FDEA201411023449.md): Wire Harness · unknown · Nov 2, 2014 · N302FE · Doug MD1030F · Engine Indicating System Wiring
  > DURING DESCENT, RECEIVED NR 3 ENGINE EXCEEDANCE CAUSED EGT HIGH. EGT TEMP FLUCTUATED BETWEEN 1000 & 1087 DEGREES, SHUTDOWN ENGINE. ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED RT UPPER AND RT LOWER THERMOCOUPLE HARNESSES. REMOVED AND REPLAC
- [SDR FDEA201410163231](https://openairdocs.org/sdr/FDEA201410163231.md): Pressure Switch · failed · Oct 16, 2014 · N302FE · Doug MD1030F · Air Intake Anti/De-Ice System
  > NR 1 ENGINE ANTI-ICE LEVEL 1 ANNUNCIATED AFTER PASSING 1000 FT IN DEPARTURE TURN. AIR TURN BACK. REMOVED AND REPLACED NR 2 ENGINE HIGH PRESSURE SWITCH. OPS CHECKED GOOD.
- [SDR FDEA201410163230](https://openairdocs.org/sdr/FDEA201410163230.md): Pressure Switch · failed · Oct 16, 2014 · N302FE · Doug MD1030F · Air Intake Anti/De-Ice System
  > NR 2 ENGINE HAD ANTI-ICE PRESSURE PASSING 1000 FT IN DEPARTURE TURN. AIR TURN BACK. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE HIGH PRESSURE SWITCH. OPS CHECKED GOOD.
- [SDR FDEA201408062092](https://openairdocs.org/sdr/FDEA201408062092.md): Sensor · faulty · Aug 6, 2014 · N302FE · Doug MD1030F · Engine RPM Indicating System
  > WHILE DESCENDING TO 6000 FEET, ENGS IDLE, NR 2 ENG RPM N1, ENG 2 EXCEEDANCE ALERT. SHUTDOWN NR 2 ENG IAW CHECKLIST. ON POST FLT FOUND NR 2 ENGINE N1 READING ERRATICALLY WITH ENGINE SHUTDOWN PEAKING @ 134.8. REMOVED AND REPLACED NR 2 FAN SPEED SENSOR IAW MM
- [SDR FDEA201405311239](https://openairdocs.org/sdr/FDEA201405311239.md): Hose · leaking · May 31, 2014 · N302FE · Doug MD1030F · Engine Thrust Reverser
  > DURING CLIMB OUT, SUFFERED NR 3 THRUST REVERSER PRESSURE FAULT. PERFORMED QRH & RETURNED TO DEPARTURE. REPLACED PNU FLEX LINE. FOUND CONNECTOR TO RT THRUST REVERSER LOCK LOOSE. TIGHTEND CONNECTOR. NO FAULTS IN AIU-1, -2 OR -3. OPS CHECKED NR 3 THRUST REVE
- [SDR FDEA201405201094](https://openairdocs.org/sdr/FDEA201405201094.md): Indicator · failed · May 20, 2014 · N302FE · Doug MD1030F · Escape Slide
  > DURING WALK AROUND INSPECTION, FOUND L1 DOOR ESCAPE SLIDE LIGHT WOULD NOT TEST. SWITCHED TEST BUTTON WITH R1 DOOR, L1 TEST BUTTON GOOD. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE TEST LIGHT ASSY.
- [SDR FDEA201309272331](https://openairdocs.org/sdr/FDEA201309272331.md): Control Unit · failed · Sep 27, 2013 · N302FE · Doug MD1030F · AC Generation System
  > DURING COCKPIT PREFLIGHT, CYCLED EMERGENCY POWER SWITCH TO ON-SELF TEST LATER FAILED. R & R EPCU REF AMM 24-08-01-4, RTS TEST PASS. OK FOR SERVICE, EMERGENCY PWR TEST PASS. ACFT ALREADY CAT 2. FROM FACT PREMATURE REMOVAL/INSTALLATION.
- [SDR FDEA201304020710](https://openairdocs.org/sdr/FDEA201304020710.md): Battery · discharged · Apr 2, 2013 · N302FE · Doug MD1030F · Battery/Charger System
  > DURING SERVICE CHECK, FOUND EMERGENCY POWER FAIL ALERT ON EAD. FOUND BOTH BATTERY VOLTAGES BELOW LIMITS. R & R BOTH BATTERIES IAW AMM 24-34-01-4. ACCOMPLISHED EMERGENCY POWER TEST, TEST PASSED. ACFT OK FOR SERVICE.
- [SDR FDEA201302260456](https://openairdocs.org/sdr/FDEA201302260456.md): Valve · failed · Feb 26, 2013 · N302FE · Doug MD1030F · Pneumatic Distribution System
  > AFTER TAKE OFF, PASSING 1500 FT. RECEIVED AURAL TRI-TONE FOR NR 2 MANIFOLD FAIL, CHECKED AIR SYS SYNOPTIC VERIFIED, REDUCED POWER TO IDLE NO HELP, STILL RED MANIFOLD INDICATIONS. RED TABS ACCOMPLISHED, RETURNED TO DEPARTURE. R & R VALVE IAW AMM 21-41-15-4
- [SDR FDEA201207242664](https://openairdocs.org/sdr/FDEA201207242664.md): Contactor · damaged · Jul 24, 2012 · N302FE · Doug MD1030F · Instrument System Wiring
  > EMERGENCY PWR OFF, LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 24-08-03-01 CATEGORY: C EXPIRATION: 01AUG12 "MEL 24-08-03-01: EMER PWR OFF LIGHT - INOP." FOUND THAT THE CENTER CONTACT BEHIND THE EMER PWR OFF LIGHT ASSY HAS NO SPRING PRESSURE. NEED TO
- [SDR FDEA201111184974](https://openairdocs.org/sdr/FDEA201111184974.md): Dimmer · failed · Nov 18, 2011 · N302FE · Doug MD1030F · Flight Compartment Lighting
  > DURING CRUISE, EXPERIENCED VERY LOUD ELECTRICAL ARCING SOUND IN OVERHEAD PANEL FOLLOWED BY THICK SMOKE FROM SAME AREA. DECLARED EMERGENCY AND DIVERTED. COMPLIED WITH QRH REMOVED SEVERAL OVERHEAD PANEL`S IN FLIGHT DECK TO LOOK FOR SOURCE OF SMOKE. INSPECTED E
- [SDR FDEA201102270791](https://openairdocs.org/sdr/FDEA201102270791.md): Charger · malfunctioned · Feb 27, 2011 · N302FE · Doug MD1030F · Battery/Charger System
  > DURING POWER TRANSFER FROM EXT TO APU, ELECT LOAD HELD FOR 15 SEC APU THEN DID AUTO SHUTDOWN. AFTER 3 MIN S/D CYCLE, APU RESTARTED. EMERGENCY POWER LT ANNUNCIATED BATTERY CHARGING REMAINED ANNUNCIATED AS WELL AS EMERGENCY POWER TEST FAIL. RESET BATTERY CHA
- [SDR FDEA201102110534](https://openairdocs.org/sdr/FDEA201102110534.md): Girt Bar · loose · Feb 11, 2011 · N302FE · Doug MD1030F · Emergency Equipment
  > DOOR L1 SLIDE GIRT BAR COMES OUT EVERYTIME DOOR IS DISARMED AND OPENED. ACTUACTED ARM/DISARM AND OPENED SEVERAL TIMES IAW MM 52-11-00-6, OP'S CHECK GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201001210210](https://openairdocs.org/sdr/FDEA201001210210.md): Adiru · malfunctioned · Jan 21, 2010 · N302FE · Doug MD1030F · Altimeter, Barometric/Encoder
  > ENROUTE, RECEIVED AMBER ALT. LIGHT IN PFD. F/O RECEIVED AMBER ALT; IAS LIGHTS ON PFD. RECEIVED A PITOT HEAT & WINDSHEAR DET FAIL ALERT LIGHT. AUTO THROTTLES & AUTOPILOT DISCONNECTED. RECEIVED SEL ELEV FEEL MAN, SEL FLAP LIM OVRD IND, SUSPECT OR ERRATIC CHE
- [SDR FDEA200907262807](https://openairdocs.org/sdr/FDEA200907262807.md): Wire Harness · damaged · Jul 26, 2009 · N302FE · Doug MD1030F · Turbine Engine System Wiring
  > CLIMB 320 TO 340 AUTO THROTTLES ENGAGED NR3 ENG EXCEEDANCE HIGH EGT 1021, REQUIRED THROTTLE REDUCTION TO MAINTAIN EGT LIMITS. COMPLIED WITH EO 8-7720-7-5001. EGT PROBES ON NR 3 CHECKED GOOD. OPENED BORESCOPE PLUGS B3-1 AND B3-2 FOR QA ON NR 3 ENG. COMPLIE
- [SDR FDEA200905061557](https://openairdocs.org/sdr/FDEA200905061557.md): Throttle Cable · binding · May 6, 2009 · N302FE · Doug MD1030F · Power Lever
  > PDX - MEM ON INITIAL DESCENT CLEARANCE, THE NR 2 THROTTLE WOULD NOT RETARD, N1 WAS APPROX 80 PERCENT ON N2. THROTTLE REMAINED FROZEN DURING ARRIVAL AND ENGINE WAS SHUTDOWN PER QRH ON DOWNWIND AT 4000 FT NR 2 THROTTLE DID FREE UP ON SHORT FINAL AND NO FURTHER
- [SDR FDEA200903241029](https://openairdocs.org/sdr/FDEA200903241029.md): Support Bracket · corroded · Mar 24, 2009 · N302FE · Doug MD1030F · Cargo/Baggage Doors
  > CENTER LOWER CARGO DOOR SPOOL BRACKET NR 2 FROM FRONT HAS DIFFERENT COLOR POWDER COMING OUT BEHIND SEALANT AND SUPPORT BRACKET, RUST COLOR. CORROSION REMOVAL PER SRM 53-50-00. HFEC BOTH HOLES TOP 2 LAYER NO CRACK INDICATION PER NDT SPM. INSTALLED FITTING RE
- [SDR 06FDEA1767](https://openairdocs.org/sdr/06FDEA1767.md): Actuator · faulted · May 9, 2006 · N302FE · Doug DC1030F · Autopilot System
  > NR 1 A/P DISENGAGE AFTER T/O. RE-ENGAGED 1 TIME WITH IMMEDIATE DISENGAGED AGAIN. PERFORMED NR 1 AND 2 FCC TEST PER MD 10-30 MM 22-00-00-5. FOUND LIB AILERON ACTUATOR AT FAULT. ALSO, NR 1 AND 2FCC AND AFSCP. REMOVED AND REPLACED 2 FCC, AFSCP AND LIB AILERO
- [SDR 06FDEA1766](https://openairdocs.org/sdr/06FDEA1766.md): Computer · malfunctioned · May 9, 2006 · N302FE · Doug DC1030 · Autopilot System
  > NR 1 A/P DISENGAGED ON CLIMBOUT. RE-ENGAGED 3 TIMES & EACH TIME IMMEDIATELY DISENGAGED AGAIN. REMOVED AND REPLACED RD FCC1. PASSED R-T-S PER MM 22-00-00-5.
- [SDR 06FDEA0100](https://openairdocs.org/sdr/06FDEA0100.md): Spring · unknown · Jan 9, 2006 · N302FE · Doug DC1030F · Flight Control System
  > FOUND CARTRIDGE SPRING ASSY ITEM 820 P/N ARH 1694-1 WITHOUT EO# 8-2780-7-4308 APPLICABLE. ACCOMPLISHED EO# 8-2780-7-4308 P1 ATTACHED, IN CONJUNCTION WITH NRC FEDEX, N00263/F160263.
- [SDR 06FDEA0099](https://openairdocs.org/sdr/06FDEA0099.md): Skin · cracked · Jan 9, 2006 · N302FE · Doug DC1030F · Trailing Edge Flaps
  > RT WING OUTBOARD FLAP FOUND 6 CRACKS ON UPPER SKIN FROM STA XOF 543 TO STA XOF 575. BURNICHED AND BLENDED INTERESTED AREAS IAW SRM 57-00-01 FIG 1A SHT 3 VOL 1, CONFIRMED 4 CRACKS STA 549 1 CRACK LONG.300" AT STA 564 FOUND 3EA CRACKS FOR TOTAL LONGEST 1" WO
- [SDR 06FDEA0098](https://openairdocs.org/sdr/06FDEA0098.md): Repair · unknown · Jan 9, 2006 · N302FE · Doug DC1030F · Wing Structure
  > FOUND LT WING SLAT NR 2 INT SKIN FOUND A FLUSH REPAIR DIM 5" BY 4.75" BY 5" XORS 264. REMOVED SLAT NR 2 LT, AND EXISTING REPAIRS, TRIMMED OUT PORTION OF INNER SKIN. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161061-3/N01061-3, F161061-5/N01061-5, F161061-7/
- [SDR 06FDEA0097](https://openairdocs.org/sdr/06FDEA0097.md): Structure · cracked · Jan 9, 2006 · N302FE · Doug DC1030F · Wing Main, Frame Structure
  > LT WING L/E FOUND 1 CRACK 1" LONG ON CHORD FIXED PANEL AT STA XORS 798. REPAIRED STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F160724-3 IAW SRM 57-10-00 FIG 49 VOL 1.
- [SDR 06FDEA0096](https://openairdocs.org/sdr/06FDEA0096.md): Repair · unknown · Jan 9, 2006 · N302FE · Doug DC1030F · Aircraft Structures
  > PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P1 FOUND DOUBLER DIMENSION 4" BY 3" RT EXTERNAL FUSELAGE STA 357 LONG 31. PERFORMED INSPECTION ON REPAIR DOUBLER IAW EA NR 8-5330-93226 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1 E3, TREATE
- [SDR 05FDEA04401](https://openairdocs.org/sdr/05FDEA04401.md): Skin · cracked · Dec 22, 2005 · N302FE · Doug DC1030 · Wing, Plate/Skin
  > LT WING L/E FOUND 1 CRACK 3.50" LONG ON SKIN AT STA XORS 505 AND 1 CRACK ON INT STRUCTURE LOWER CHORD FIXED PANEL. CLEANED AREA IAW M/M 12-22-01. REMOVED REFUELING DOOR IAW SRM 51-31-01 PAGE 36/41 VOL 2. REMOVED FASTENERS, WEB AND SKIN AS REQUIRED, REMOVED
- [SDR 05FDEA04400](https://openairdocs.org/sdr/05FDEA04400.md): Floorbeam · misrepaired · Dec 22, 2005 · N302FE · Doug DC1030 · Fuselage Main, Floor Beam
  > AFT CARGO COMPT AT STA 1902 FOUND 1 FLOORBEAM REPAIRED FROM X 55 LT TO X -55 RT AT Z-83 WITH 1 SPLICE AND 1 WEB. STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. PERFORMED INSPECTION AND REPORTED VALUE ON ATTACHED SHEET. PERFORMED CONDUCTIVITY INSPECTION REPORT
- [SDR 05FDEA04354](https://openairdocs.org/sdr/05FDEA04354.md): Repair · unknown · Dec 16, 2005 · N302FE · Doug DC1030 · Aircraft Structures
  > FOUND DOUBLER LENGTH 9" WIDTH 8" ON RT EXT FUSELAGE AT STA 879 LONG 36. REMOVED AND REPLACED REPAIR IAW 1-109812697-7 AND SRM 53-20-00 FIG 6 SHT 5- 6 VOL 1 AND FEDEX EA# 8-5310-93218. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160401-2 INNER EXTERNAL DOUBL
- [SDR 05FDEA04353](https://openairdocs.org/sdr/05FDEA04353.md): Repair · none · Dec 16, 2005 · N302FE · Doug DC1030 · Aircraft Structures
  > FOUND MAIN CARGO COMPT STA 1921 Z 31 BY 92 FOUND 1 NEW SECTION OF FRAME 33" LONG WITH 2 SPLICE. PERFORMED INSPECTION ON FRAME IAW SRM 53-30-00 FIG 5 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINT ON STRIPPED AREA I
- [SDR 05FDEA04311](https://openairdocs.org/sdr/05FDEA04311.md): Repair · unknown · Dec 14, 2005 · N302FE · Doug DC1030 · Wing Structure
  > RT WING SLAT NR 2 FOUND DOUBLER REPAIR ON UPPER SKIN T/E OB SIDE DIM 3 INCHES BY 3 INCHES. REMOVED REPAIR IAW SRM 51-35-01 PAGE 13 AND SRM 51-33-01 PAGE 34/47. CLEANED AREAS AND REMOVED PART IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDI SPM08. FOUND
- [SDR 05FDEA04310](https://openairdocs.org/sdr/05FDEA04310.md): Doubler · damaged · Dec 14, 2005 · N302FE · Doug DC1030 · Fuselage Main, Structure
  > PERFORMED INSPECTION IAW EO 8-5100-7-5001-P1 FOUND DOUBLER DIM 15 INCHES BY 14 INCHES LT EXT FUS STA 595 LONG 46 TO LONG 48. PERFORMED A GVI OF REPAIR IAW SRM 53-20-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1D E3.
- [SDR 05FDEA04309](https://openairdocs.org/sdr/05FDEA04309.md): None · none · Dec 14, 2005 · N302FE · Doug DC1030 · Standard Practices/Structures
  > LT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.25 INCHES BY 1.75 INCHES AT STA XORS 532. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.
- [SDR 05FDEA04308](https://openairdocs.org/sdr/05FDEA04308.md): Repair · none · Dec 14, 2005 · N302FE · Doug DC1030 · Aircraft Structures
  > LT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.75 INCHES BY 2.75 INCHES AT STA XORS 521. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.
- [SDR 05FDEA04312](https://openairdocs.org/sdr/05FDEA04312.md): Angle · cracked · Dec 14, 2005 · N302FE · Doug DC1030 · Leading Edge Devices
  > LT WING SLAT NR 4 FOUND 1 CRACK 1" LONG ON ANGLE AT STA XORS 506. REPLACED CLIP IAW MD-10-30 M/M 27-80-01-7 FIG 401 SHT 1 AND PERFORMED ADJUSTMENT IAW MD-10-30 M/M 27-80-01-7 FIG 408 SHT 1.
- [SDR 05FDEA04272](https://openairdocs.org/sdr/05FDEA04272.md): Repair · misinstalled · Dec 13, 2005 · N302FE · Doug DC1030F · Fuselage Main, Plate/Skin
  > DISCREPANCY PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND 1 DOUBLER DIMENS 13" BY 10" RT EXT FUSELAGE STA 665 LONG 41. REMOVED DOUBLER IAW SRM 51-30-00 AND SRM 51-35-02 STRIPPED PAINT IAW SRM 51-21-01 VOL 2. REMOVED FINGER DOUBLER EXTERNAL IAW SRM 51-3
- [SDR 05FDEA04271](https://openairdocs.org/sdr/05FDEA04271.md): Repair · unknown · Dec 13, 2005 · N302FE · Doug DC1030F · Aircraft Structures
  > FWD LOWER CARGO DOOR FOUND EXTERNAL DOUBLER FROM STA 885 TO STA 959 DIM 11 X 12 INCHES. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 6 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F161770-3, DOUBLER IAW SRM 52-10-00 FIG 6 VOL 1.
- [SDR 05FDEA04270](https://openairdocs.org/sdr/05FDEA04270.md): Repair · unknown · Dec 13, 2005 · N302FE · Doug DC1030F · Aircraft Structures
  > PERFORMED INSPECTION IAW EO# 8-5100-7-5001-1D FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1.
- [SDR 05FDEA04269](https://openairdocs.org/sdr/05FDEA04269.md): Intercostal · cracked · Dec 13, 2005 · N302FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT AT STA 879 RT AT LONG 39 AFTER REMOVAL INTERCOSTAL WITH N/R C40124 FOUND ON STRUT 1 CRACK 2.50" LONG. REMOVED PLATE IAW SRM 51-33-01 PAGE 34/47 VOL 2. TRIMMED OUT CRACKED FLANGE. FABRICATED PART IAW DETAIL PART TRAVELER F161706/3 IAW SRM 53-
- [SDR 05FDEA04142](https://openairdocs.org/sdr/05FDEA04142.md): Repair · damaged · Dec 5, 2005 · N302FE · Doug DC1030F · Elevator Structure
  > DISCREPANCY IN THE UPPER SURFACE OF RT DETACHABLE ELEVATOR AT STA XE 80 FOUND 1EA REPAIR DOUBLER 3.5 INCH DIA. PERFORMED A GVI OF REPAIR IAW SRM 55-00-01 FIG 3 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P, RESTORED PAINT ON STRIP
- [SDR 05FDEA04140](https://openairdocs.org/sdr/05FDEA04140.md): Repair · unknown · Dec 5, 2005 · N302FE · Doug DC1030F · Elevator Structure
  > LEFT OUTBOARD ELEVATOR REPAIR ASSESSEMENT FOUND 1EA EXT DOUBLER ON LOWER SIDE AT XE 345 DIMENIONS 7 X 4.5 INCH. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. RESTORED
- [SDR 05FDEA04139](https://openairdocs.org/sdr/05FDEA04139.md): Repair · unknown · Dec 5, 2005 · N302FE · Doug DC1030F · Wing, Plate/Skin
  > RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH 236 DIMENIONS 3.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P. RESTORED PAINT ON STRIPPED AREA IA
- [SDR 05FDEA04138](https://openairdocs.org/sdr/05FDEA04138.md): Repair · unknown · Dec 5, 2005 · N302FE · Doug DC1030F · Wing, Plate/Skin
  > RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENIONS 8.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2. RESTORED PAINT ON STRIPPED AREA I
- [SDR 05FDEA04137](https://openairdocs.org/sdr/05FDEA04137.md): Repair · unknown · Dec 5, 2005 · N302FE · Doug DC1030F · Wing, Plate/Skin
  > RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 155 DIMENIONS 3.25 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IA
- [SDR 05FDEA04135](https://openairdocs.org/sdr/05FDEA04135.md): Repair · unknown · Dec 5, 2005 · N302FE · Doug DC1030F · Elevator Structure
  > INBOARD LT ELEVATOR UPPER SIDE FOUND 1 EXTERNAL DOUBLER REPAIR DIA 3" AT XE 160. PERFORMED INSPECTION OF REPAIR DOUBLER IAW SRM 55-00-01 VOL 1 FIG 3. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW
- [SDR 05FDEA04136](https://openairdocs.org/sdr/05FDEA04136.md): Repair · unknown · Dec 5, 2005 · N302FE · Doug DC1030F · Elevator Structure
  > FOUND UPPER INBOARD LT ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR BETWEEN XE 240 AND XE 191 DIMENS. 45" BY 8". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAIN
- [SDR 05FDEA04134](https://openairdocs.org/sdr/05FDEA04134.md): Repair · proper · Dec 5, 2005 · N302FE · Doug DC1030F · Elevator Structure
  > UPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 70 DIMENSION 4" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPE
- [SDR 05FDEA04133](https://openairdocs.org/sdr/05FDEA04133.md): Repair · proper · Dec 5, 2005 · N302FE · Doug DC1030F · Elevator Structure
  > UPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 60 DIMENSION 7" BY 6.5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 VOL 1 FIG 8 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EONR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AR
- [SDR 05FDEA04132](https://openairdocs.org/sdr/05FDEA04132.md): Repair · proper · Dec 5, 2005 · N302FE · Doug DC1030F · Fuselage Main, Structure
  > DISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P1 FOUND DOUBLER DIMENS 14" BY 4" RT, EXTERNAL FUSELAGE STA 959 LONG 40 TO LONG 42. PERFORMED A GVI OF REPAIR IAW SRM 53-50-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100
- [SDR 05FDEA04130](https://openairdocs.org/sdr/05FDEA04130.md): Repair · proper · Dec 5, 2005 · N302FE · Doug DC1030F · Fuselage Main, Structure
  > DISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P2 FOUND DOUBLER DIMENS 12" BY 7.5" EXTERNAL FUSELAGE AT STA 1370 LONG 51 RT TO 51 LT. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-51
- [SDR 05FDEA04129](https://openairdocs.org/sdr/05FDEA04129.md): Repair · proper · Dec 5, 2005 · N302FE · Doug DC1030F · Trailing Edge Flaps
  > DISCREPANCY LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 7.75" BY 4.75" ON LOWER SKIN AT STA XIFH 133. PERFORMED A GVI OF REPAIR IAW EA NR 8-5710-90133 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 AND TREATED STRIPPED AREA IAW SRM 51-21-
- [SDR 05FDEA04128](https://openairdocs.org/sdr/05FDEA04128.md): Repair · proper · Dec 5, 2005 · N302FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > DISCREPANCY IN THE AFT FUSELAGE SECTION ZONE 316 AT STA Y 2140 FOUND 1 REPAIR ANGLE ON THE FRAME'S CAP AT X10 SIZE 10" X 2.5". PERFORMED A GVI OF REPAIR IAW SRM 53-30-00 VOL 1 FIG 2 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2D E3, R

Next page: https://openairdocs.org/deregistered/N302FE-2024-02-03/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 = 'N302FE' AND deregistration_id = 'N302FE-2024-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N302FE-2024-02-03/reports

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