# Service difficulty reports: N564FE, cancelled Mar 2, 2024

A list on [N564FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N564FE-2024-03-02.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 3 · 106 reports

- [SDR FDEA201607162482](https://openairdocs.org/sdr/FDEA201607162482.md): Engine · failed · Jul 16, 2016 · N564FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > UPON ADVANCING POWER FOR TAKEOFF, FELT A RUMBLING IN THE RUDDER PEDALS. ABORTED T/O AT AT 10 KTS. TURNED OFF RUNWAY, ANOTHER ACFT ADVISED SEEING FLAMES FROM THE NR 2 ENGINE. SHUTDOWN ENGINE, BLEW BOTH FIRE BOTTLES. REMOVED NR 2 ENG PER WORK CARD 71T1101
- [SDR FDEA201607032231](https://openairdocs.org/sdr/FDEA201607032231.md): Fire Warning · false activation · Jul 3, 2016 · N564FE · Doug MD1010F · Fire Detection
  > DURING PREFLIGHT, CARGO FIRE LOWER FWD, LEVEL 3 ALERT DISPLAYED. INVESTIGATED AND FOUND CARGO DOOR CLOSED. COMPLIED WITH QRH. R & R NR 105LB, LOWER CARGO COMPARTMENT FIRE EXTINGUISHING CONTAINER.
- [SDR FDEA201511173654](https://openairdocs.org/sdr/FDEA201511173654.md): Sensor · failed · Nov 17, 2015 · N564FE · Doug MD1010F · Pneumatic Indicating System
  > AT 370 RECEIVED LEVEL 1 HIGH STAGE 3 OFF ALERT, FOLLOWED BY LEVEL 1 MANIFOLD 3 FAIL ALERT. PERFORMED QRH, RAN THROTTLE IN IDLE. REPLACED NR 2 ENG HIGH STAGE TEMP SENSOR IAW AMM 36-11-01-2. OPERATIONS CHECKED GOOD. PERFORMED PSC 1, 2 & 3 RTS IAW AMM 36-10-0
- [SDR FDEA201508082517](https://openairdocs.org/sdr/FDEA201508082517.md): Sliding Window · unsecure · Aug 8, 2015 · N564FE · Doug MD1010F · Flight Compartment Windows
  > REJECTED TAKEOFF, AIR NOISE FROM CAPTAIN`S WINDOW. CHECKED LATCH. LATCH APPEARED CLOSED & LOCKED. THE CAPTAIN PUSHED THE LOCKING ARM FWD ABOUT.750 ON HIS SLIDING WINDOW. NO REPORTS FROM THE FLIGHT CREW OF ANY NOISE COMING FROM CAPTAIN`S SLIDING WINDOW.
- [SDR FDEA201508062490](https://openairdocs.org/sdr/FDEA201508062490.md): Unknown · malfunctioned · Aug 6, 2015 · N564FE · Doug MD1010F · Engine Oil Indicating System
  > LEVEL 2 ENG 1 OIL FILTER ALERT DURING CLIMB PASSING FL 200. ALL OIL PRESS & TEMP INDICATIONS WERE NORMAL, NO VIBRATION. REDUCED THROTTLE TO IDLE. LEVEL 2 ALERT REMAINED. SHUTDOWN NR 1 ENG IAW QRH GUIDANCE, NO OTHER INDICATIONS. ENG 1 CONTINUED TO WINDMILL
- [SDR FDEA201507112199](https://openairdocs.org/sdr/FDEA201507112199.md): Slide · blown · Jul 11, 2015 · N564FE · Doug MD1010F · Escape Slide
  > R1 SLIDE BLOWN ON ARRIVAL. REMOVED DEPLOYED SLIDE & RAFT ASSEMBLY AS REQUIRED IAW AMM 25-61-07-4. RESET & SERVICED RI DOOR AIR RESERVOIR AS REQUIRED IAW AMM 51-10-01-2. INSTALLED NEW EVACUATION SLIDE & RAFT ASSEMBLY AS REQUIRED IAW AMM 25-61-01-2. DOOR CHE
- [SDR FDEA201503100790](https://openairdocs.org/sdr/FDEA201503100790.md): Wire · broken · Mar 10, 2015 · N564FE · Doug MD1010F · Landing Gear System Wiring
  > DURING CLIMB OUT APPROXIMATELY FIVE MINUTES AFTER TAKEOFF RECEIVED A LEVEL 2 BRAKE OVERHEAT ALERT. CONFIGURATION PAGE SHOWED LT TRUCK RT AFT TIRE TEMP, BRAKE NR 6, RISING RAPIDLY THRU 800 DEGREES, THEN WENT TO A X. COMPLIED WITH QRH & EXTENDED GEAR FOR 10
- [SDR FDEA201502260600](https://openairdocs.org/sdr/FDEA201502260600.md): Anti-Ice System · unknown · Feb 26, 2015 · N564FE · Doug MD1010F · Pneumatic Indicating System
  > DURING DESCENT WITH ENGINE & WING ANTI - ICE ON INITIALLY RECEIVED A NR 3 MANIFOLD FAILURE LIGHT SELECTED. WING ANTI - ICE OFF, NR 3 MANIFOLD FAIL LIGHT REMAINED ON, BUT NO LEVEL3, AIR MANIFOLD 3 FAIL ALERT, SYNOPTIC SHOWED RED FAILURE INDICATION OF MANIFO
- [SDR FDEA201501300390](https://openairdocs.org/sdr/FDEA201501300390.md): Switch · stuck · Jan 30, 2015 · N564FE · Doug MD1010F · Passenger/Crew Doors
  > RAMP CREW REPORTED THAT AFTER CLOSING L1 DOOR, IT WOULD NOT OPEN ELECTRICALLY. ON INSPECTION FOUND DOOR OPEN SWITCH PLUNGER STUCK IN THE OPEN POSITION. LUBED AND CYCLED PLUNGER SEVERAL TIMES. RAN L1 DOOR THROUGH FULL CYCLE SEVERAL TIMES IAW AMM 52-10-01-5-0,
- [SDR FDEA201409302871](https://openairdocs.org/sdr/FDEA201409302871.md): Support · corroded · Sep 30, 2014 · N564FE · Doug MD1010F · Aerodynamic Fairings
  > RIGHT AFT BODY FAIRING AFT SUPPORT SHOWING EXFOLIATION CORROSION. REPAIRED IAW EA 8-5320-T0311923.
- [SDR FDEA201409262790](https://openairdocs.org/sdr/FDEA201409262790.md): Skin · corroded · Sep 26, 2014 · N564FE · Doug MD1010F · Ailerons
  > LEFT WING INBD AILERON UPPER SURFACE SHOWS CORROSION. LT INBD AILERON R & R IAW N00135 & MM 27-10-01-4.
- [SDR FDEA201409252786](https://openairdocs.org/sdr/FDEA201409252786.md): Skin · worn · Sep 25, 2014 · N564FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE LE WORN. REPAIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201409232742](https://openairdocs.org/sdr/FDEA201409232742.md): Skin · gouged · Sep 23, 2014 · N564FE · Doug MD1010F · Leading Edge Devices
  > LEFT WING NR 5 SLAT LOWER SURFACE HAS DEEP GOUGE BY NR 11 SLAT TRACK. REPAIRED IAW SRM 57-00-01 VOL1 FIG 4 SHEET 2.
- [SDR FDEA201409232737](https://openairdocs.org/sdr/FDEA201409232737.md): Skin · dented · Sep 23, 2014 · N564FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBD FLAP VANE TOP SURFACE HAS SHARP DENT. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201409232735](https://openairdocs.org/sdr/FDEA201409232735.md): Vane · delaminated · Sep 23, 2014 · N564FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT FLAP VANE LE INBD OF NR 3 TRACK HAS SMALL SECTION OF DELAMINATION. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201409222704](https://openairdocs.org/sdr/FDEA201409222704.md): Skin · damaged · Sep 22, 2014 · N564FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT LOWER FLAP SURFACE SKIN HAS HAIL DAMAGE. FABRICATED DOUBLER IAW SRM 57-10-00 FIG 85 SHEET 2.
- [SDR FDEA201409222703](https://openairdocs.org/sdr/FDEA201409222703.md): Doubler · cracked · Sep 22, 2014 · N564FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING FIXED LE INNER SKIN DOUBLER HAS APPROX 10 INCH CRACK AT STATION XORS 570. INSTALLED.020 TITANIUM DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.
- [SDR FDEA201409192678](https://openairdocs.org/sdr/FDEA201409192678.md): Shear Tie · corroded · Sep 19, 2014 · N564FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT AT STATION 1781, BULKHEAD TO SKIN SHEAR TIE HAS EXFOLIATION CORROSION AT L48R. R & R SHEAR TIE IAW 51-30-00 VII.
- [SDR FDEA201409082533](https://openairdocs.org/sdr/FDEA201409082533.md): Floor Support · cracked · Sep 8, 2014 · N564FE · Doug MD1010F · Fuselage Main, Floor Beam
  > LEFT CORNER OF FLOOR SUPPORT HAS A 1.25 INCH CRACK EMANATING FROM TOP FASTENER ON FRAME VERTICAL FWD FLANGE. PERFORMED REPAIR IAW SRM 53-30-00 FIG 7, VOL 1
- [SDR FDEA201402270418](https://openairdocs.org/sdr/FDEA201402270418.md): Strut · cracked · Feb 27, 2014 · N564FE · Doug MD1010F · Nose/Tail Landing Gear Strut/Axle
  > FOUND NOSE GEAR LEAKING FLUID. INVESTIGATION FOUND ROUGHLY 15 INCH CRACK IN STRUT FROM TOP OF SERVICE POINT TO DOWN TO FRONT OF STRUT. INSTALLED SERVICEABLE NOSE LANDING GEAR ASSEMBLY IAW AMM 32-21-01-4. OPS & LEAK CHECKED GOOD.TAXIED AIRCRAFT PER
- [SDR FDEA201401260202](https://openairdocs.org/sdr/FDEA201401260202.md): Mechanism · dirty · Jan 26, 2014 · N564FE · Doug MD1010F · Landing Gear Selector
  > HAD 3 GEAR UNSAFE, AFTER 2 CYCLES OF GEAR HANDLE, RAN QRH. ON THIRD ATTEMPT GOT 3 GREEN. FOUND EXCESSIVE FRICTION IN THE LONGITUDINAL AXIS OF THE LG CONTROL LEVER. CLEANED & LUBRICATED THE LG CONTROL MECHANISM IAW MD-10-10 AMM 32-31-02-7.
- [SDR FDEA201312243037](https://openairdocs.org/sdr/FDEA201312243037.md): Control Unit · faulty · Dec 24, 2013 · N564FE · Doug MD1010F · Brake Anti-Skid Section
  > LEFT ANTI-SKID FAIL. CREW STATED DURING DEBRIEF ALERT APPEARED AT GEAR EXTENSION, DID GO AROUND & HAD NO ALERT ON THE SECOND GEAR EXTENSION. ASCU SHOWS ASCU FAULTED AT THE TIME OF THE FIRST GEAR EXTENSION. SYS TESTING NORMAL AT THE GATE WITH NO ALERTS. R
- [SDR FDEA201210013520](https://openairdocs.org/sdr/FDEA201210013520.md): Sleeve · damaged · Oct 1, 2012 · N564FE · Doug MD1010F · Engine Thrust Reverser
  > ON TAXI, ADVISED BY THE TOWER THAT A PIECE OF OUR ENGINE COWL HAD FALLEN OFF. FOUND NR 2 ENGINE RT THRUST REVERSER COWL DAMAGED AND A LARGE SECTION MISSING. REMOVED NR 2 RT FAN REVERSER HALF IAW W/C 78T3101R-2. INSTALLED NR 2 ENGINE RT REVERSER HALF AND
- [SDR FDEA201208263178](https://openairdocs.org/sdr/FDEA201208263178.md): Skin · misrepaired · Aug 26, 2012 · N564FE · Doug MD1010F · Leading Edge Devices
  > LEFT WING NR 6 SLAT MISREPAIRED. REPAIRED IAW EA 8-5750-160700, REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201205231960](https://openairdocs.org/sdr/FDEA201205231960.md): Skin · corroded · May 23, 2012 · N564FE · Doug MD1010F · Rudder, Plate/Skin
  > LOWER AFT RUDDER, FWD RT SIDE HAS AREA OF SURFACE CORROSION. REPAIRED LWR AFT RUDDER ON RT SIDE IAW SRM 55-10-00 AND EA 8-5540-157335.
- [SDR FDEA201108153279](https://openairdocs.org/sdr/FDEA201108153279.md): Lamp · inoperative · Aug 15, 2011 · N564FE · Doug MD1010F · Emergency Lighting
  > ENTRY DOOR LIGHTED EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS, DIM ILLUMINATION. RELAMPED THE LT EXIT LIGHT'S IAW SMP CHECKED OK.
- [SDR FDEA201104041309](https://openairdocs.org/sdr/FDEA201104041309.md): Light · inoperative · Apr 4, 2011 · N564FE · Doug MD1010F · Escape Slide
  > WHILE DOING PREFLIGHT FOUND R1 DOOR SLIDE TEST LIGHT NOT WORKING. REPLACED SLIDE PACK LIGHT SW ASSY, SLIDE LIGHT OPS. GOOD, IAW AMM 25-61-03-2. (CLOSED)
- [SDR FDEA201009023237](https://openairdocs.org/sdr/FDEA201009023237.md): Coalescer Bag · dirty · Sep 2, 2010 · N564FE · Doug MD1010F · Humidity Control System
  > AT FL360, AFTER COCKPIT TEMP ADJUSTMENT-STRONG SMOKE ODOR FOLLOWED BY LARGE AMOUNT OF SMOKE IN COCKPIT. FOLLOWED QUICK REF HANDBOOK FOR SMOKE AND FUMES. EMERGENCY DECLARED AND LANDED. REF MM 21-53-00-7 & JRH C/W PACK BURN ON ALL 3 ACFT. PACKS WITH ENG BLE
- [SDR FDEA201008012753](https://openairdocs.org/sdr/FDEA201008012753.md): Angle · corroded · Aug 1, 2010 · N564FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > CTR PIT SUMP DRAIN COMPT SHEAR TIE HAS CORROSION AT STA. 1761 APPROX. BETWEEN S- 51L TO S-51R. FOUND CORROSION OUT OF LIMITS AFTER BLENDING, REMOVED AND REPLACED SUPPORT ANGLE, SHEAR TIES IAW SRM 51-31-01, MAJOR REPAIR.
- [SDR FDEA201007292724](https://openairdocs.org/sdr/FDEA201007292724.md): Support · corroded · Jul 29, 2010 · N564FE · Doug MD1010F · Fuselage Main, Structure
  > AFT CARGO COMPT LOWER FRAME SUPPORT HAS CORROSION AT STA. 1841 BETWEEN S-49R AND S-50R. REMOVED AND REPLACED FRAME SUPPORT AT STA 1841 BETWEEN S-49R AND S-50R IAW SRM 51-21-01 AND SRM 53-01-00, FIG. 8 MAJOR REPAIR.
- [SDR FDEA201007282690](https://openairdocs.org/sdr/FDEA201007282690.md): Shear Tie · corroded · Jul 28, 2010 · N564FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > CENTER PIT SUMP DRAIN COMPT. SHEAR TIE IS CORRODED AT AFT SURFACE AT STA. 1781 BETWEEN S-47R TO S-48R. REMOVED AND REPLACED CENTER PIT SUMP DRAIN COMPT. SHEAR TIE IAW SRM 53-30-00, FIG. 10, MAJOR REPAIR.
- [SDR FDEA201007172575](https://openairdocs.org/sdr/FDEA201007172575.md): Seat Track · damaged · Jul 17, 2010 · N564FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT SEAT TRACK LBL 107 FS 1701 TO 1841 HAS 4 EA LOBES WORN. FABRICATED SEAT TRACK, HAT AND SPLICE USING TRAVELER T10/844703 AND T10/84470544705 FROM MATERIALS 7075-T6511, 7075-T6.050 AND 7075-T6 EXT. BATCH NUMBERS 0001665654, 0001610155 AN
- [SDR FDEA201007162563](https://openairdocs.org/sdr/FDEA201007162563.md): Seat Track · damaged · Jul 16, 2010 · N564FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO SEAT TRACK FS 1731 TO 1721, LBL 28 HAS 2 LOBES PROTRUDING UPWARD AND ADDITIONAL LOBES DISTORTED. R & R DAMAGED SEAT TRACK SECTION AT LBL 28 FS 1721-1771 IAW SRM 51-31-01 AND SRM 53-70-00. CLASSIFIED AS A MAJOR REPAIR.
- [SDR FDEA201007162562](https://openairdocs.org/sdr/FDEA201007162562.md): Floorbeam · cracked · Jul 16, 2010 · N564FE · Doug MD1010F · Fuselage Main, Floor Beam
  > MAIN DECK STA 475, LBL 77 TO 107, FLOORBEAM IS CRACKED/DAMAGED. FABRICATED FLOORBEAM SEC REPAIR FROM 7075-T6.071 BATCH NR 183113 IAW SRM 53-00-01, FIG 9, SHEET 7. TREATED AND PRIMED REPAIR IAW SRM 51-21-01. INSTALLED REPAIR IAW SRM 51-31-01. PAINTED AREA I
- [SDR FDEA200909263389](https://openairdocs.org/sdr/FDEA200909263389.md): Sensor · failed · Sep 26, 2009 · N564FE · Doug MD1010F · Engine RPM Indicating System
  > FLT 3707. NR 2 ENGINE ROLLED BACK ON TAKEOFF, MAX N1 WAS 84 PERCENT, ENGINE FAIL LIGHT ON. CKED VIA'S AND HAD NR 2 ENG N1 FAILED MSG -PROBABLE CAUSE ENG 2 TACHOMETER. REPLACED NR 2 ENG FAN SPEED SENSOR/N1 TACH PER AMM 77-11-01-2 OPS CKS NRML, RAN ENG TO T/
- [SDR FDEA200909113286](https://openairdocs.org/sdr/FDEA200909113286.md): Coalescer Bag · odor · Sep 11, 2009 · N564FE · Doug MD1010F · Humidity Control System
  > AFTER STARTING APU AND TURNING ON THE PACKS. HAD SMOKE COMING OUT OF DUCTS. R & R NR 3 PACK COALESCER BAGS, RAN APU, CLEARED FUMES FROM AIR CONDITIONING DUCTS. RAN NR 2 PACK IAW AMM AMM 21-00-01-5. NO SMOKE NOTED. RAN ALL 3 ENGINES AT HIGH POWER FOR 45 MINU
- [SDR FDEA200909103285](https://openairdocs.org/sdr/FDEA200909103285.md): Plug · leaking · Sep 10, 2009 · N564FE · Doug MD1010F · Hydraulic Pump (Electric/Engine), Main
  > WHEN APU WAS STARTED AND APU BLEED TURNED ON, CABIN FILLED WITH SMOKE, TURNED OFF BLEEDS FOUND HYD FLUID RUNNING FROM AFT DRAIN HOLE INTO APU INLET. FOUND REV MOTOR PUMP S/O VALVE M1-165 DRIPPING IN AFT COMPT PN 148995, AIPC 29-12-60-03, FACT 10SEP09 06:58
- [SDR FDEA200907172661](https://openairdocs.org/sdr/FDEA200907172661.md): Warning Light · false activation · Jul 17, 2009 · N564FE · Doug MD1010F · Landing Gear Position and Warning
  > GEAR UNSAFE WARNING DURING GEAR EXTENSION. GA PROCEDURE. ACCOMPLISHED QRH PROCEDURE ACCOMPLISHED WITH NORMAL GEAR EXTENSION - LEFT MAIN. NO CURRENT FAULTS LOGGED, CHECKED RIGGING IN PSEU AND SENSORS ARE WITHIN LIMITS PER AMM 32-61-15-5. PERFOMED R-T-S AND P
- [SDR 08FDEA03715](https://openairdocs.org/sdr/08FDEA03715.md): Panel · damaged · Sep 3, 2008 · N564FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON APRON HAS EDGE DAMAGE AT THE FWD END WHERE THE LT FAN COWL MATES. REPAIRED NR 2 FAN COWL LT APRON IAW E.A. 8-5480-123629.
- [SDR 08FDEA03642](https://openairdocs.org/sdr/08FDEA03642.md): Vane · delaminated · Aug 29, 2008 · N564FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP VANE; INBOARD LOWER SKIN IS DELAMINATED. REMOVED DELAMINATED INBOARD LOWER SKIN ON LEFT OUTBOARD FLAP VANE INBOARD END. FABRICATED SKIN PLUG & REPAIR DOUBLER. PREPPED FOR BONDING; HOT BONDED REPAIR. ALODINED AREA & EDGE SEALED DOUBLER;
- [SDR 08FDEA03629](https://openairdocs.org/sdr/08FDEA03629.md): Skin · cracked · Aug 28, 2008 · N564FE · Doug MD1010F · Leading Edge Devices
  > RIGHT NR 1 SLAT LOWER SURFACE SKIN IS CRACKED AT A FASTENER HOLE, TRAILING EDGE APPROX 1 INCH FROM THE INBD END. REMOVED RIGHT WING NR 1 SLAT IAW AMM 27-80-01-4. OPENED SKIN FOR ACCESS. REMOVED THE CRACKED SECTION. FABRICATED A REPAIR, INSTALLED REPAIR A
- [SDR 08FDEA03599](https://openairdocs.org/sdr/08FDEA03599.md): Frame · corroded · Aug 26, 2008 · N564FE · Doug MD1010F · Fuselage Main, Frame
  > FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO EXISTING FRAME BEING CORRODED BEYOND LIMITS AT STA 1501. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DAC DWG AEA 0273; REV "G". LOCATED AND DRILLED AEA 0273-3 FRAME AND AEA 0273-5 SHEAR TIE. ALODINED AND
- [SDR 08FDEA03528](https://openairdocs.org/sdr/08FDEA03528.md): Longeron · corroded · Aug 21, 2008 · N564FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LONGERON 51 L RIGHT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON 51 L END FITTING P/N AYB 7020-2 IAW DWG NR AYB 7020.
- [SDR 08FDEA03527](https://openairdocs.org/sdr/08FDEA03527.md): Longeron · corroded · Aug 21, 2008 · N564FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LONGERON 51 L LEFT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON END FITTING P/N AYB 7020-2 IAW BAC DWG NR AYB7020.
- [SDR 08FDEA03505](https://openairdocs.org/sdr/08FDEA03505.md): Longeron · corroded · Aug 19, 2008 · N564FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LONGERON 52 AT STA 1480 IN THE CENTER LANDING GEAR COMPARTMENT HAS CORROSION. REMOVED DAMAGED SECTION OF LONGERON 52 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND DRILLED NEW SECTION OF LONGERON 52 AND 2 SPLICES IAW DWG AYB 7013 AND SRM 53-00-01; FIG 9; PG 32;
- [SDR 08FDEA03445](https://openairdocs.org/sdr/08FDEA03445.md): Frame · corroded · Aug 15, 2008 · N564FE · Doug MD1010F · Fuselage Main, Frame
  > FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO BEING CORRODED BEYOND LIMITS. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DWG AEA 0273; REV "G". LOCATED AND DRILLED AEA 0273-3 FRAME AND AEA 0273-5 SHEAR TIE. ALODINED AND PRIMED IAW SRM 51-21-01; PGS
- [SDR 08FDEA03398](https://openairdocs.org/sdr/08FDEA03398.md): Bulkhead · corroded · Aug 13, 2008 · N564FE · Doug MD1010F · Fuselage Main, Bulkhead
  > THE CENTER WHEEL WELL SKIN HAS VARIOUS AREAS OF CORROSION FROM STA 1521 THRU 1380; BETWEEN LONGERON 51L TO LONGERON 51R. REPAIRED THE CENTER WHEEL WELL SKIN IAW FEDEX EA 8-5330-117008 " FUSELAGE, UNDER WING BARREL BELLY SKIN CORROSION, REPAIR". REMOVED AND R
- [SDR 08FDEA03444](https://openairdocs.org/sdr/08FDEA03444.md): Skin · cracked · Aug 12, 2008 · N564FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RIGHT SIDE FUSELAGE SKIN AT STA 322 IS CRACKED 10 INCHES ABOVE THE FINGER DOUBLERS. REMOVED FIRST OFFICERS SEAT IAW AMM 25-11-01-4. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-20-00; FIG 6; VOL I. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. INSTALL
- [SDR 08FDEA03377](https://openairdocs.org/sdr/08FDEA03377.md): Longeron · corroded · Aug 11, 2008 · N564FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 51L FROM BODY STA 1441 TO 1461. REMOVED DAMAGED SECTION OF LONGERON 51L FROM FS 1430 TO 1520 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND DRILLED NEW SECTION OF LONGERON 51L AND 2 EA SPLICES IAW DWG AYB 7013 AND SRM 53-00-01; FIG 9; PG
- [SDR 08FDEA03265](https://openairdocs.org/sdr/08FDEA03265.md): Longeron · corroded · Aug 5, 2008 · N564FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > NR 1 AIR CONDITIONING COMP FUSELAGE SKIN, ANGLES; INTERCOSTAL WEB AND FASTENERS ARE CORRODED BETWEEN STA 562 AND STA 593; LONGERON 43L IMMEDIATELY OUTBOARD OF THE EXHAUST BOX. REPLACED CORRODED THROUGH LONGERON SECTION ACA 3353-3 LEFT BY SPLICING IN A NEW PI

Next page: https://openairdocs.org/deregistered/N564FE-2024-03-02/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 = 'N564FE' AND deregistration_id = 'N564FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N564FE-2024-03-02/reports

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