# Service difficulty reports: N556FE, cancelled Apr 13, 2024

A list on [N556FE, cancelled Apr 13, 2024](https://openairdocs.org/deregistered/N556FE-2024-04-13.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 · 213 reports

- [SDR FDEA201210263757](https://openairdocs.org/sdr/FDEA201210263757.md): Battery · inoperative · Oct 26, 2012 · N556FE · Doug MD1010F · Escape Slide
  > ESCAPE SLIDE LOW PRESSURE INDICATOR PRESS TO TEST LIGHT WILL NOT TEST. R & R BATTERIES, REF AMM 25-61-01-2. OPS CHECKED GOOD.
- [SDR FDEA201210113597](https://openairdocs.org/sdr/FDEA201210113597.md): Coalescer Bag · contaminated · Oct 11, 2012 · N556FE · Doug MD1010F · Humidity Control System
  > OIL FUMES APPEAR TO BE COMING FROM NR 3 PACK. PACK SHUTOFF, BLEED ON. OIL QUANITY STABLE IAW AMM 49-00-00-2 INSPECTED APU BLEED AIR OUTLET AND LOAD BLEED VALVE FOR OIL, NONE FOUND. CHANGED ALL WATER COALESCER BAGS IAW AMM 24-54-03-2. WITH ISOLATION VALVES
- [SDR FDEA201208213093](https://openairdocs.org/sdr/FDEA201208213093.md): Skin · cracked · Aug 21, 2012 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT FWD LT SIDE OF NOSE GEAR W/W CUTOUT. COMPLIED WITH EA 8-5350-157364 & REPAIRED AREA USING SRM 53-50-00.
- [SDR FDEA201208213092](https://openairdocs.org/sdr/FDEA201208213092.md): Skin · cracked · Aug 21, 2012 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT FWD RT SIDE OF NOSE GEAR W/W CUTOUT REPAIRED USING SRM 53-50-00 AS A REFERENCE.
- [SDR FDEA201108113201](https://openairdocs.org/sdr/FDEA201108113201.md): Engine · stalled · Aug 11, 2011 · N556FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > ON CLIMBOUT, PASSING FL 290 FELT 2 FIRM JOLTS WITH YAW TO THE LT ENG INDICATIONS NORMAL IN COCKPIT. FELT LIKE COMPRESSOR STALL ON NR 1 ENG. ENG RPM'S AT THE TIME WERE ATS CET 101 PERCENT. REMOVED AND REPLACED NR 3 ENG. LEAK AND OPS CHECKED GOOD. ACFT OK
- [SDR FDEA201105191877](https://openairdocs.org/sdr/FDEA201105191877.md): Connector · unsecure · May 19, 2011 · N556FE · Doug MD1010F · Escape Slide
  > R1 DOOR SLIDE LIGHT DOES NOT TEST. RESEATED CONNECTOR ON BACK OF PRESS TO TEST SWITCH R1 DOOR. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201103311265](https://openairdocs.org/sdr/FDEA201103311265.md): Oil System · leaking · Mar 31, 2011 · N556FE · Doug MD1010F · Turbine Engine Oil System
  > DURING CRUISE, NR 2 ENG OIL QTY STARTED DROPPING 1 GAL EVERY 8 MIN. WHEN QUANTITY HIT 3 AND AMBER, WE ALSO GOT AN ENG 2 OIL PRESSURE LOW ALERT AND IT STAYED ON WITH ENG THROTTLE AT IDLE. SHUTDOWN ENGINE IAW QRH. CREW VERBAL ON DEBRIEF: ENGINE WAS ALREADY
- [SDR FDEA201103191081](https://openairdocs.org/sdr/FDEA201103191081.md): Shunt · loose · Mar 19, 2011 · N556FE · Doug MD1010F · DC Generating System
  > EMERG PWR TEST FAIL ON PREFLIGHT EPCU FAULTS "BATTERY/INTFC" REF FIM 24-30-19. TERMINAL ON SHUNT S4-1 LOOSE AND ARCING. S4-1 REPLACED SHUNT S4-1, REF WDM 24-08-01, SHT 3 AND SWPM. ALSO R & R EPCU REF AMM. FINAL CLOSED.
- [SDR FDEA201102040475](https://openairdocs.org/sdr/FDEA201102040475.md): Frame · cracked · Feb 4, 2011 · N556FE · Doug MD1010F · Fuselage Main, Frame
  > CAC, FWD PRESSURE BULKHEAD RT SIDE MAIN FRAME CRACKED ALLTHE WAY THROUGH AT BS 1157 BETWEEN LONGERON 27R AND 28R. REMOVED DAMAGED PARTS, FABRICATED NEW PARTS AND TREATED PARTS IN ACCORDANCE WITH EA 8-5310-142572. INSTALLED PARTS AND SEALED AS REQUIRED PER S
- [SDR FDEA201012294761](https://openairdocs.org/sdr/FDEA201012294761.md): Control Unit · failed · Dec 29, 2010 · N556FE · Doug MD1010F · Central Display
  > DURING CRUISE FL360 F/O'S MCDU BLANKED OUT FOR APPROX 1 MINUTE THEN CAME BACK ON. THEN WE SMELLED ELECTRICAL FIRE/FUMES. PULLED F/O, MULTI-FUNCTION DISPLAY UNIT NR 2 CB RT EMERGENCY AC BUSS, ODOR/FUMES WENT AWAY. R & R THE MULTIFUNCTION CONTROL UNIT IAW
- [SDR FDEA201011274501](https://openairdocs.org/sdr/FDEA201011274501.md): Wire Harness · malfunctioned · Nov 27, 2010 · N556FE · Doug MD1010F · Light System Wiring
  > EMERGENCY EXIT SIGNS INOP. RELEASED FOR SERVICE IAW MEL: 33-50-02, WHEN SHAKING HARNESS BY L1 DOOR LIGHTS COME ON, BUT UNABLE TO FIND EXACT CAUSE AT THIS TIME. REPLACED L1 DOOR "EXIT" LIGHT ASSY. ACCOMPLISHED ADJ AND TEST IAW MM 33-50-00-5.
- [SDR FDEA200812025047](https://openairdocs.org/sdr/FDEA200812025047.md): Warning System · activated · Dec 2, 2008 · N556FE · Doug MD1010F · Landing Gear Position and Warning
  > LANDING MEM, 18R 3 UNSAFE (RED) GEAR LIGHTS WITH GEAR HANDLE DOWN, 3 UNSAFE ON CONFIG PAGE, QRH PROCEDURE DEPLOY ALT GEAR EXTENSION AND RECEIVED 3 GREEN SAFE (CONFIG AND GEAR). NOSEWHEEL STEERING RIGHT LIMITED TO 25 DEG.
- [SDR 08FDEA04266](https://openairdocs.org/sdr/08FDEA04266.md): Pressure Panel · cracked · Oct 8, 2008 · N556FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS A CRACK ALONG UPPER EDGE ACROSS THREE RIVETS ENDING AT STIFFENER, FWD OF PNEUMATIC DUCT. (VERIFIED CRACK USING LFEC) REPAIRED CRACK AS REQ., REF. EA 8-5310-118303. SEE JPF WORK STEP SIGNOFFS.
- [SDR 08FDEA04270](https://openairdocs.org/sdr/08FDEA04270.md): Web · cracked · Oct 8, 2008 · N556FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS CRACK COMING FROM HOLE FOR THERMOCOUPLE. THIS CRACK HAS BEEN STOP DRILLED TWICE AND IS CRACKED PAST SECOND STOP DRILL. (VERIFIED CRACKED USING LFEC) REPAIRED CRACK AS REQ., REF. EA 8-5310-118303. WORK
- [SDR 07FDEA02558](https://openairdocs.org/sdr/07FDEA02558.md): Bulkhead · corroded · Jul 20, 2007 · N556FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 1521 LONGERON 50R TO 49R. REMOVED CORROSION ON T-CHORD IAW MD/DC10 SRM 51-21-01 VOL II PAGE 1, DAC DWG AEA 0018,ORIG. THICKNESS.200 REMAINING THICKNESS.177,.023 REMOVED. REMOV
- [SDR 07FDEA02526](https://openairdocs.org/sdr/07FDEA02526.md): Shear Tie · corroded · Jul 19, 2007 · N556FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > CLG WHEEL WELL CAVITY, CORROSION ON SHEAR TIE/LONGERON AT STA 15012 LONGERON 50L. REMOVED, FABRICATED AND INSTALLED NEW SHEAR-TIE/ FRAME IAW MD/DC10 SRM51-33-01 VOL II, 53-00-01 FIG 1B VOLI, 51-35-01 VOLII AND DWG AEA0273 REV G.
- [SDR 07FDEA02525](https://openairdocs.org/sdr/07FDEA02525.md): Frame · corroded · Jul 19, 2007 · N556FE · Doug MD1010F · Fuselage Main, Frame
  > CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 15121, BETWEEN LONGERON 51L AND 52. REMOVED, REPLACED AND INSTALLED 2 EACH ANGLES AT 51L TO 52 AT FS 1521 IAW MD/DC10 SRM 51-33-01 VOL II PAGE 1.
- [SDR 07FDEA02524](https://openairdocs.org/sdr/07FDEA02524.md): Frame · corroded · Jul 19, 2007 · N556FE · Doug MD1010F · Fuselage Main, Frame
  > CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENTIAL ANGLE AT STA 152 LONGERON 50R TO 49R. REMOVED, FABRICATED AND INSTALLED 4 EACH ANGLES 49R TO 50R IAW MD/DC10 SRM 51-33-01 VOLII AND 51-35-01 VOLII PAGE 1.
- [SDR 07FDEA02523](https://openairdocs.org/sdr/07FDEA02523.md): Skin · dented · Jul 19, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT SKIN DENTED AT APPROXIMATELY THE 5:00 POSITION ON FRAME AND IS 18 INCHES OF RVSM (CENTER PLATE). THIS SDR REPLACES (SDR#07-2123) REPAIRED SKIN IAW EA 8-55330-112937 FUSELAGE-SKIN REPAIR AT STA 851-913 L36R-L48R.
- [SDR 07FDEA02522](https://openairdocs.org/sdr/07FDEA02522.md): Seat Track · corroded · Jul 19, 2007 · N556FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO1840. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW MD/DC10 SRM 51-31-01 VOLII AND 51-21-01 VOLII AND DWG AGA3855.
- [SDR 07FDEA02516](https://openairdocs.org/sdr/07FDEA02516.md): Skin · corroded · Jul 18, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CLG WHEEL WELL CAVITY, CORROSION ON SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW MD/DC10 SRM 51-35-01 VOLII. SKIN REPLACED ON N/R N00616 EA8-5330-112939 (FUSELAGE SKIN REPAIR AT STA 1381- 1531, L48
- [SDR 07FDEA02514](https://openairdocs.org/sdr/07FDEA02514.md): Longeron · corroded · Jul 18, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 51L. REMOVED, FABRICATED AND INSTALLED NEW END FITTINGS IAW MD/DC10 SRM51-33-01 VOLII.
- [SDR 07FDEA02494](https://openairdocs.org/sdr/07FDEA02494.md): Longeron · corroded · Jul 16, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON LONG END FITTINGS AT STA 1521 LONG 48L CLG WHEEL WELL. REMOVED AND REPLACED L48L END FITTINGS IAW DC/MD-10 SRM 51-33-01 VOL. II.
- [SDR 07FDEA02493](https://openairdocs.org/sdr/07FDEA02493.md): Longeron · corroded · Jul 16, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CLG WHEEL WELL CAVITY CORROSION ON LONGERON END FITTING STA 1501 TO STA 1521 LONGERON 51L TO 52L REMOVED AND REPLACED LONGERON END FITTING L52R IAW DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 07FDEA02492](https://openairdocs.org/sdr/07FDEA02492.md): Intercostal · corroded · Jul 16, 2007 · N556FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CLG WHEEL WELL CAVITY CORROSION ON INTERCOSTAL ABOVE LONGERON 52 R STA 1381 TO 1401. REMOVED AND REPLACED INTERCOSTAL IAW DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 07FDEA02491](https://openairdocs.org/sdr/07FDEA02491.md): Skin · corroded · Jul 16, 2007 · N556FE · Doug DC1010F · Fuselage Main, Plate/Skin
  > CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW DC-10/MD-10 SRM 51-35-01 VOL II.
- [SDR 07FDEA02490](https://openairdocs.org/sdr/07FDEA02490.md): Longeron · corroded · Jul 16, 2007 · N556FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END FITTING AT STA 1521, L48R CLG WHEEL/WELL. REMOVED AND REPLACED LONGERON END FITTINGS L48R IAW DC-10/MD-10 SRM 51-35-01 VOL. II.
- [SDR 07FDEA02489](https://openairdocs.org/sdr/07FDEA02489.md): Skin · corroded · Jul 16, 2007 · N556FE · Doug DC1010F · Wing, Plate/Skin
  > UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II.
- [SDR 07FDEA02488](https://openairdocs.org/sdr/07FDEA02488.md): Skin · corroded · Jul 16, 2007 · N556FE · Doug DC1010F · Wing, Plate/Skin
  > UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II.
- [SDR 07FDEA02481](https://openairdocs.org/sdr/07FDEA02481.md): Longeron · corroded · Jul 13, 2007 · N556FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL 1 FIG 1A. REMOVED AND REPLACED LONGERON SECTION IAW MD10-10 SRM 53-00-01 FIG 9 VOL 1, AND 51-35-01 VOL 2. FABRICATED LONGE
- [SDR 07FDEA02484](https://openairdocs.org/sdr/07FDEA02484.md): Longeron · corroded · Jul 13, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L REMOVED CORROSION ON LONGERON END FITTING AND FOUND TO BE WITHIN LIMITS IAW DC/MD10-10 SRM53-00-01 FIG 1B VOL 1. ORIGINAL THICKNESS 0.130" MATERIAL LOSS 0.007", MATERIA
- [SDR 07FDEA02483](https://openairdocs.org/sdr/07FDEA02483.md): Longeron · corroded · Jul 13, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL 1 FIG 1A. REMOVED AND REPLACED LONGERON SECTION IAW MD10-10 SRM 53-00-01 FIG 9, VOL 1, AND 51-35-01 VOL 2. FABRICATED LONG
- [SDR 07FDEA02418](https://openairdocs.org/sdr/07FDEA02418.md): Seat Track · gouged · Jul 10, 2007 · N556FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT RBL - 8 AT STA 1199 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. FABRICATED SEAT TRACK AND SPLICE REPAIR IAW DC/MD 10 SRM 53- 70-00 VOL I FIG 5. INSTALLED IAW DC/MD 10 SRM 51-31-01 VOL II.
- [SDR 07FDEA02417](https://openairdocs.org/sdr/07FDEA02417.md): Seat Track · gouged · Jul 10, 2007 · N556FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT LBL - 8 BETWEEN STA 1681 AND 1701 IS GOUGED BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VOL I PG 3. FABED SEAT TRACK AND 2 SPLICE HAT AND 2 PLATES IAW DC/MD 10 SRM 53-70-00 V
- [SDR 07FDEA02416](https://openairdocs.org/sdr/07FDEA02416.md): Seat Track · gouged · Jul 10, 2007 · N556FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT RBL-27, AT STA 1059 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VOL I PGS 1-6A AND DC/MD 10 SRM 51-21-01 VOL II PGS 1-46.
- [SDR 07FDEA02288](https://openairdocs.org/sdr/07FDEA02288.md): Skin · dented · Jun 26, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE SKIN FWD OF R-1 DOOR SILL. REMOVED DENT, FABRICATED AND INSTALLED SKIN AND FILLER IAW DC/MD10 SRM 53-20-00 VOL I FIG 6 SHT 4, 53-10-00 VOL II PAGE 75 AND 53-20-00 VOL I PAGE 23.
- [SDR 07FDEA02287](https://openairdocs.org/sdr/07FDEA02287.md): Skin · corroded · Jun 26, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE CIRCUMFERENTIAL ANGLE AT STA.1521, BETWEEN LONGERON 52 AND 51R. [07-13-07] REMOVED INTERCOSTAL AT LONG 51R, FS 1501-1521 IAW SRM 51-33-01 VOL2 PG1. REMOVED CORROSION ON TEE CHORD FS 1521 FROM LONG 51R-52R IAW S
- [SDR 07FDEA02286](https://openairdocs.org/sdr/07FDEA02286.md): Bulkhead · corroded · Jun 26, 2007 · N556FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 1521, BETWEEN LONGERON 51L AND 52. [07-17-07] REMOVED,FABRICATED AND INSTALLED IAW SRM 51-33-01.
- [SDR 07FDEA02285](https://openairdocs.org/sdr/07FDEA02285.md): Bulkhead · corroded · Jun 26, 2007 · N556FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CLG - WHEEL WELL CAVITY,CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 152, LONGERON 50R TO 49R. [07-17-07] REMOVED,FABRICATED AND INSTALLED 4 EACH END FITTINGS 49R TO 50R IAW SRM 51-33-01 VOL II AND 51-35-01 VOL II PAGE 1.
- [SDR 07FDEA02282](https://openairdocs.org/sdr/07FDEA02282.md): Skin · corroded · Jun 26, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L. [07-13-07] REMOVED LONGERON 49L END FITTING IAW DC/MD10-10 SRM 51-33-01 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. ORIG THICKNESS 0.130", MATERIAL LOSS 0.
- [SDR 07FDEA02262](https://openairdocs.org/sdr/07FDEA02262.md): Skin · corroded · Jun 22, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR SURFACE AT STA 1441, LONGERON 51R TO 51L. SKIN SECTION FROM 1401 TO 1541 IS BEING REPLACED ON N/R N00616 ATTACHED EA 8-5330- 112939/FUSELAGE-SKIN SPLICE AT STA.1381-1531,L48LTO L48R-REPAIR.
- [SDR 07FDEA02263](https://openairdocs.org/sdr/07FDEA02263.md): Skin · corroded · Jun 22, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE SKIN BETWEEN LONGERON 51L AND 52 STA 1350 TO 1370. CLEANED AREA IAW DC/MD10 SRM51-21-01 PARA.22 VOL. II. NO CORROSION NOTED. MECH 7951 QC281
- [SDR 07FDEA02250](https://openairdocs.org/sdr/07FDEA02250.md): Longeron · corroded · Jun 21, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 52 STA 1461 TO 1501,CLG WHEEL WELL CAVITY. [07-13-07] FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 51-33-01 VOL 2. FABRICATED NEW LONG SECTION IAW DAC DWG A4B7013 REV AC, AND REPAIR SPLICES IAW MD10-10 SRM 53-00-01 FIG 9, VOL 1. REMOV
- [SDR 07FDEA02249](https://openairdocs.org/sdr/07FDEA02249.md): Longeron · corroded · Jun 21, 2007 · N556FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CLG WHEEL WELL CAVITY, CORROSION ON LONGERON 51R STA 1441 TO 1501. [07-13-07] FOUND TO BE WITHIN LIMITS IAW MD10-10 SRM 53-00- 01 VOL 1, ORIGINAL THICKNESS 0.150, MATERIAL LOSS 0.010, REMAINING MATERIAL 0.140. SAT 1481 - 1521 FOUND TO BE OUT OF LIMITS I
- [SDR 07FDEA02247](https://openairdocs.org/sdr/07FDEA02247.md): Angle · dented · Jun 21, 2007 · N556FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF LOWER TORQUE BOX WEB FOR SKIN REPLACEMENT ON N/R N00337, FOUND INNER CHORD ANGLE ADA0055-7 DENTED AT STA 886 JUST ABOVE L41 RIGHT. [07-17-07] REPAIRED PER EA 8-5310-112940.
- [SDR 07FDEA02147](https://openairdocs.org/sdr/07FDEA02147.md): Skin · corroded · Jun 15, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN INTERIOR AT STA 1441 TO 1481, LONGERON 50L TO 50R, CENTER LANDING GEAR WHEEL WELL CAVITY. [07-13-07] REMOVED AND REPLACED SKIN WITH NEW SECTION FS1391-1521, LONGERON 48L - 48R IAW FEDEX EA 8-5330-112939 (FUSELAGE SKIN REPAIR A
- [SDR 07FDEA02146](https://openairdocs.org/sdr/07FDEA02146.md): Skin · corroded · Jun 15, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CENTER LANDING GEAR WHEEL WELL,CORROSION ON FUSELAGE SKIN AT STA 1501 TO 1521, LONGERON 51R TO 50R. [07-17-07] REPLACED ON N00616 WITH EA 8-5330-112939.
- [SDR 07FDEA02123](https://openairdocs.org/sdr/07FDEA02123.md): Skin · dented · Jun 13, 2007 · N556FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT SKIN DENTED AT APPROXIMATELY 5:00 POSITION ON FRAME AND IS WITHIN 18 INCHES OF RVSM (CENTER) PLATE. [07-17-07] REPAIRED SKIN IAW EA 8-5330-112937 MAJOR REPAIR.
- [SDR 07FDEA02122](https://openairdocs.org/sdr/07FDEA02122.md): Skin · corroded · Jun 13, 2007 · N556FE · Doug MD1010F · Ailerons
  > LT O/B AILERON BULGING AT FASTENERS ON SKIN. [07-17-07] REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II. MAJOR REPAIR.
- [SDR 07FDEA02121](https://openairdocs.org/sdr/07FDEA02121.md): Seat Track · corroded · Jun 13, 2007 · N556FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO 1840. [07-17-07] REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-31-01 VOL II, 51-21-01 VOL II AND DWG. 3855. MINOR REPAIR.

Next page: https://openairdocs.org/deregistered/N556FE-2024-04-13/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 = 'N556FE' AND deregistration_id = 'N556FE-2024-04-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N556FE-2024-04-13/reports

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