# Service difficulty reports: N370FE, cancelled May 9, 2018

A list on [N370FE, cancelled May 9, 2018](https://openairdocs.org/deregistered/N370FE-2018-05-09.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 4 · 156 reports

- [SDR FDEA201609173291](https://openairdocs.org/sdr/FDEA201609173291.md): Former · cracked · Sep 17, 2016 · N370FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RIGHT WING L/E FORMER CRACKED AT XOS 703, LOWER END. REPAIRED L/E FORMER, WEB, ANGLE IAW SRM 57-00-01, FIG 10, VOL I. THIS REPAIR IS A CATEGORY-A, MAJOR REPAIR.
- [SDR FDEA201511113573](https://openairdocs.org/sdr/FDEA201511113573.md): Warning System · false activation · Nov 11, 2015 · N370FE · Doug MD1010F · Door Warning System
  > WHEN CLOSING UP PRIOR TO PUSH, R1 DOOR DISARMED. LIGHT REMAINS ILLUMINATED WHEN DOOR IS ARMED.
- [SDR FDEA201511013433](https://openairdocs.org/sdr/FDEA201511013433.md): Seat Track · damaged · Nov 1, 2015 · N370FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LOBE DAMAGED, INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. INSTALLED FLOOR PANELS & CARGO LOADING SYS IAW AMM 53-21-08-2, ANCRA 25-50-66.
- [SDR FDEA201507072163](https://openairdocs.org/sdr/FDEA201507072163.md): Combining Box · defective · Jul 7, 2015 · N370FE · Doug MD1010F · Central Display
  > TWENTY MINUTES AFTER DEPARTURE STARTED TO NOTICE LIGHT SMOKE, HAZE & ODOR. DETERMINED SOURCE MOST LIKELY FROM HUD WITH EFVS ON. TURNED EFVS OFF & ODOR, SMOKE & HAZE STOPPED. RELEASED FOR SERVICE IAW MEL 31-61-04-01 CATEGORY C, EXPIRATION 17JUL 15. HUD SYS
- [SDR FDEA201507032151](https://openairdocs.org/sdr/FDEA201507032151.md): Coalescer Bag · dirty · Jul 3, 2015 · N370FE · Doug MD1010F · Humidity Control System
  > AT FL 380 WE ENCOUNTERED ACRID SMOKE IN THE COCKPIT. PERFORMED QRH PROCEDURE TO CLEAR SMOKE. SMOKED CLEARED AFTER 10 - 15 MINS. REPLACED OLD COALESCER BAGS WITH NEW BAGS IAW AMM 21-54-03-2. REFER TO WRI 26-12 4858 FOR FURTHER DETAILS & INSTRUCTIONS.
- [SDR FDEA201506171915](https://openairdocs.org/sdr/FDEA201506171915.md): Battery · failed · Jun 17, 2015 · N370FE · Doug MD1010F · Emergency Lighting
  > DURING EMER LIGHT TEST LEVEL 1, EMER BAT 1 LO. REMOVED & INSTALLED EMER LIGHTING BATTERY POWER SUPPLY. OK FOR CONTINUED SERVICE.
- [SDR FDEA201506101744](https://openairdocs.org/sdr/FDEA201506101744.md): Adiru · failed · Jun 10, 2015 · N370FE · Doug MD1010F · Attitude and Direction Data System
  > NOTICED APPROXIMATELY 2000 FT DIFFERENCE BETWEEN NR 1 AND 2 MCDU DURING PROFILE DESCENT WITH F/O FLYING. SWITCHED AUTOPILOTS TO GET BACK ON PROFILE. AFTER BLOCK-IN IRU NR 2 SHOWED 14.8 DIRIFT & 15 GROUND SPEED. REPLACED THE NR 2 ADIRU, ACOMPLISHED T
- [SDR FDEA201503211042](https://openairdocs.org/sdr/FDEA201503211042.md): Indicator · damaged · Mar 21, 2015 · N370FE · Doug MD1010F · Passenger Compartment Lighting
  > SOCKET ASSEMBLY FOR R1, DOOR DISARM, LIGHT IS BROKEN. R & R INDICATOR ASSEMBLY IAW SMP 20-00-00. OPERATIONS NORMAL.
- [SDR FDEA201503211041](https://openairdocs.org/sdr/FDEA201503211041.md): Indicator · damaged · Mar 21, 2015 · N370FE · Doug MD1010F · Passenger Compartment Lighting
  > SOCKET ASSEMBLY FOR L1 DOOR DISARM LIGHT IS BROKEN. R & R LT FWD ENTRY DOOR DISARM LIGHT SOCKET ASSEMBLY IAW LMMS SM 52-11-0 S1-S2 & IPC 52-11--75-02 ITEM 420. TESTED NORMAL ON GND.
- [SDR FDEA201502280614](https://openairdocs.org/sdr/FDEA201502280614.md): Charger · inoperative · Feb 28, 2015 · N370FE · Doug MD1010F · Battery/Charger System
  > EMERGENCY POWER TEST FAILED TWICE DURING PREFLIGHT. ASSOCIATED BATTERY CHARGER INOPERATIVE MINUTES LATER. REPLACED BATTERY CHARGER IAW MM 24-34-02-2-0. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201410072998](https://openairdocs.org/sdr/FDEA201410072998.md): Skin · chafed · Oct 7, 2014 · N370FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT OTBD FLAP VANE UPPER SURFACE OTBD OF OTBD TRACK HAS CHAFED. RT OTBD FLAP VANE UPPER SURFACE REPAIRED IAW SRM 57-53-01. EA 8-5750-T0312136 REV NO PS P1 TITLE WINGS FLIGHT SURFACES RT OTBD FLAP VANE UPPER SURFACE CHAFED RSC TRACKING ISSUED. MAJOR REPAI
- [SDR FDEA201410062991](https://openairdocs.org/sdr/FDEA201410062991.md): Skin · chafed · Oct 6, 2014 · N370FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING INBD FLAP VANE INBD UPPER SURFACE THE REPAIR DOUBLER IS CHAFED WITH PAINT OVER. REPAIRED RT WING INBD FLAP VANE UPPER SURFACE IAW SRM 57-00-01, SRM 51-71-00 & SRM 51-23-10. EA 8-5750-T0312137 REV NO PS P1 TITLE WINGS FLIGHT SURFACES RT WING INBD F
- [SDR FDEA201410012883](https://openairdocs.org/sdr/FDEA201410012883.md): Panel · cracked · Oct 1, 2014 · N370FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON PRE COOLER PANEL 437DR RIB STIFFENERS TOP & BOTTOM SIDES, INCLUDING FWD & AFT FLANGES, FOUND CRACKED WELDED AREAS. VERIFIED PANEL 437DR SECONDARY STRUCTURE IAW EA 8-5450-T0311730 STEP 1. WELDED RIB STIFFENERS TOP & BOTTOM SIDES & FWD & AFT FLA
- [SDR FDEA201410012882](https://openairdocs.org/sdr/FDEA201410012882.md): Duct · cracked · Oct 1, 2014 · N370FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > PANEL 437DR, NR 1 PYLON HEAT EXCHANGE DUCT, INNER WALL CRACKED. REMOVED FASTENERS IAW SRM 51-35-01 FOR ACCESS TO WELD SUPPORT ANGLES. INSTALLED FASTENERS IAW SRM 51-35-01. WELDED NR 1 PYLON HEAT EXCHANGE DUCT ON T14 1095275 IAW EA 8-5450-T0311727 REV NR PS
- [SDR FDEA201409302870](https://openairdocs.org/sdr/FDEA201409302870.md): Skin · dented · Sep 30, 2014 · N370FE · Doug MD1010F · Elevator, Plate/Skin
  > LEFT INBD ELEVATOR TE UPPER SURFACE HAS DENT. EVALUATED DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 VOL 1 FIG 8 L = 2 INCHES, W = 4 INCHES. FABRICATED DOUBLER & FILLER IAW SRM 55-10-00 FIG 8 PG 15. INSTALLED FASTENERS IAW SRM 51-36-01. REPAIRED LT INBD
- [SDR FDEA201409302867](https://openairdocs.org/sdr/FDEA201409302867.md): Panel · cracked · Sep 30, 2014 · N370FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 3 ENG PYLON PANEL 487DL HAS CRACK LOWER LT CORNER OF PRE COOLER BOX, MARKED. REMOVED FASTENERS TO ACCESS CRACK IAW SRM 51-31-01. WELDED CRACK ON T14 1095277. REINSTALLED FASTENERS IAW SRM 51-31-01. ACCOMPLISHED WELD REPAIR IAW EA 8-5450-T0311731 REV
- [SDR FDEA201409302866](https://openairdocs.org/sdr/FDEA201409302866.md): Panel · cracked · Sep 30, 2014 · N370FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 3 ENG PYLON PANEL 487DL HAS CRACK FWD LOUVER RADIUS, MARKED. WELDED CRACK ON T14 1095278 ON NR 3 ENG PYLON PANEL 487DL MAT 321 DPS 10.225, AMS 5L80 ROD & ACCOMPLISHED IAW EA 8-5450-T0311732 REV NO PS P1. MINOR REPAIR.
- [SDR FDEA201409292856](https://openairdocs.org/sdr/FDEA201409292856.md): Skin · damaged · Sep 29, 2014 · N370FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR OUTER SKIN BOTTOM FWD CORNER HAS A NOTCH CUT OUT. TEMP REPAIR, FABRICATED DOUBLER MAT 2024-T3.071C, BATCH 2021540 IAW SRM 52-10-00 FIG 12A SHEET 1. INSTALLED DOUBLER IAW SRM 52-10-00. ACCOMPLISHED EA 8-5210-T0311872 RSC FOR TRACKING. MAJOR REPAIR
- [SDR FDEA201409272827](https://openairdocs.org/sdr/FDEA201409272827.md): Doubler · damaged · Sep 27, 2014 · N370FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING LE PANEL 518GB HAS ONE EACH ELONGATED FASTENER HOLE ON PANEL CUT OUT. R & R LT WING LE ACCESS PANEL 518GB LANDING DOUBLER WITH NEW PART. FABRICATED FROM 7075-T6, 0.090C BN 1885277 IAW 57-21-01 FIG 7 ITEM 33 & SRM 51-31-01. MAJOR REPAIR..
- [SDR FDEA201409242760](https://openairdocs.org/sdr/FDEA201409242760.md): Longeron · corroded · Sep 24, 2014 · N370FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LOWER FWD CARGO COMPARTMENT LONGERON 52 CORRODED BETWEEN STATION 735 - 755. REPAIRED IAW SRM 53-10-00 FIG 2 SHEET 1. REMOVED CORROSION ON LONGERON & FOUND TO BE OUT OF LIMITS IAW SRM 53- 00-01 FIG 1 B. MAJOR REPAIR.
- [SDR FDEA201409192688](https://openairdocs.org/sdr/FDEA201409192688.md): Floorbeam · corroded · Sep 19, 2014 · N370FE · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM AFT FLANGE IS EXFOLIATED AT STATION 1841, PARALLEL TO LONGERON 51L. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. REPAIRED IAW SRM 53-00-01 FIG 7, MATERIAL USED 7075- T6 063 1498-200 PO 0002031082. MAJOR REPAIR.
- [SDR FDEA201409172643](https://openairdocs.org/sdr/FDEA201409172643.md): Floorbeam · cracked · Sep 17, 2014 · N370FE · Doug MD1010F · Fuselage Floor Panel
  > MCD FLOORBOARD STATION 1909 - 2007, RBL 36 HAS CRACKS. FABRICATED FLOOR PANEL ON T14 1093394, BATCH 2663757 IAW SRM 51-61-01 / SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201409142608](https://openairdocs.org/sdr/FDEA201409142608.md): Fitting · corroded · Sep 14, 2014 · N370FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FRAME LOWER FWD CORNER FITTING IS CORRODED. REMOVED AND REPLACED THE CORNER FITTING IAW SRM 51-31-01. ADJUSTED, SAFTIED OPS CHECKED GOOD IAW AMM 52-33-00-0. MAJOR REPAIR.
- [SDR FDEA201408062101](https://openairdocs.org/sdr/FDEA201408062101.md): Light · inoperative · Aug 6, 2014 · N370FE · Doug MD1010F · Lighting System
  > 1L DOOR LIGHT DOES NOT TEST. CHANGED BATTERIES IN L1 DOOR IAW SMP.
- [SDR FDEA201406141450](https://openairdocs.org/sdr/FDEA201406141450.md): Skin · cracked · Jun 14, 2014 · N370FE · Doug MD1010F · Wing, Plate/Skin
  > DURING POST FLIGHT, FOUND A CRACK ON THE LT WING LE AT NR 4 SLAT, OTBD TRACK CUT OUT, LOWER, INBD RADIUS. HFEC INSPECTED SUSPECTED IAW NDTSPM 06-10 01 & VERIFIED THE CRACK TO BE A 3/8 - 1/2 INCH LONG. CUT OUT DAMAGED AREA IAW SRM. VERIFIED CRACK REMOVED US
- [SDR FDEA201406141452](https://openairdocs.org/sdr/FDEA201406141452.md): Skin · cracked · Jun 14, 2014 · N370FE · Doug MD1010F · Wing, Plate/Skin
  > WHILE PERFORMING FCD, FOUND A CRACK ON NR 1 INBD SLAT TRACK SKIN CUT OUT LT WING. VERIFIED CRACK USING HFEC IAW NDTSPM 06-10-01. CRACK 1/2 INCH IN LENGTH. REMOVED CRACK. COMPLIED WITH HFEC INSPECTION, NO CRACKS FOUND. REPAIRED IAW EA 8-5710-F0308207.
- [SDR FDEA201301180146](https://openairdocs.org/sdr/FDEA201301180146.md): Sensor · malfunctioned · Jan 18, 2013 · N370FE · Doug MD1010F · Landing Gear Position and Warning
  > ON GEAR RETRACTION, AFTER TAKEOFF, RT MAIN GEAR DID NOT INDICATE UP AND LOCK ON BOTH THE PRIMARY AND SECONDARY INDICATORS. ON TOUCHDOWN, IT FEELS LIKE RT GEAR BOTTOMS OUT AS THE AIRPLANE SETTLES TO THE RUNWAY. CHECK WIRES IAW WDM 32-61-01, 32-61-03 AND TROU
- [SDR FDEA201301170125](https://openairdocs.org/sdr/FDEA201301170125.md): Sensor · inoperative · Jan 17, 2013 · N370FE · Doug MD1010F · Landing Gear Retraction/Extension System
  > WITH THE LANDING GEAR HANDLE UP, THE RT GEAR INDICATION NOT UP AND LOCK IN BOTH THE PRIMARY AND SECNDARY INDICATORS. (LIGHT RED) PERFORMED VISUAL INSP OF RT MLG UPLOCK PROX SENSOR AND NO DEFECTS NOTED, PSEU RTS PASSES NORMALLY, CHECKED PSEU SENSOR READOUT UN
- [SDR FDEA201206232320](https://openairdocs.org/sdr/FDEA201206232320.md): Fuel Control · malfunctioned · Jun 23, 2012 · N370FE · Doug MD1010F · Fuel Control/Turbine Engines
  > FLEX PWR SET FOR 50 PERCENT, THROTTLES ADVANCED SMOOTHLY WHEN AUTOFLT SELECTED TO THE APPROPRIATE REDUCED PWR CHEVRON INDICATED SETTINGS ON THEN 1 GUAGE. THROTTLES CLAMPED NORMALLY PRIOR TO 80KTS. AFTER 80 KTS THE NR 3 ENGINE BEGAN NOTICEABLY SURGING WITH N
- [SDR FDEA201108023064](https://openairdocs.org/sdr/FDEA201108023064.md): Door · inoperative · Aug 2, 2011 · N370FE · Doug MD1010F · Passenger/Crew Doors
  > DOOR L1 HAD NO POWER TO CLOSE AT CLOSEUP AND PUSHBACK. DOOR OPS CHECKED GOOD IAW MM 52-10-01-2-0.
- [SDR FDEA201108023063](https://openairdocs.org/sdr/FDEA201108023063.md): Lens · missing · Aug 2, 2011 · N370FE · Doug MD1010F · Emergency Lighting
  > DURING SERVICE CHECK, FOUND L1 DOOR INSIDE FWD UPPER EMERGENCY LIGHT LENS COVER MISSING. INSTALLED NEW L1 DOOR INSIDE FWD UPPER EMERGENCY LIGHT LENS COVER IAW STANDARD PRACTICE.
- [SDR FDEA201106152255](https://openairdocs.org/sdr/FDEA201106152255.md): Engine · malfunctioned · Jun 15, 2011 · N370FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > RTO BELOW 80 KNOTS FOR LVL 1 ENG 2 EXCEEDANCE ALERT. MAX N2 101.1. PREVIEWED QRH FOR LVL1 AND RTO. ADVISED MX. RETURNED TO GATE. COMPLIED WITH VISUAL INSP OF NR 2 ENG EXHAUST AREA IAW AMM 72-00-00-6, NO DAMAGE NOTED. INSPECTED WHEELS TIRES BRAKES AND MLG D
- [SDR FDEA201104261632](https://openairdocs.org/sdr/FDEA201104261632.md): Connector · corroded · Apr 26, 2011 · N370FE · Doug MD1010F · Engine Oil System Wiring
  > WE RECEIVED AN ENG 2 OIL FILTER, LEVEL 2 ALERT. FOLLOWING QRH ENG 2 WAS SHUTDOWN. REMOVED AND REPLACED THE SCAVANGE AND MAIN LUBE OIL FILTERS, NO CONTAMINATION WAS FOUND REF. AMM MD10-79-20-02 AND 79-20-01, LEAK CHECK WAS GOOD. COMPLETED A 5 MINUTES GROU
- [SDR FDEA201011234466](https://openairdocs.org/sdr/FDEA201011234466.md): Cable · bent · Nov 23, 2010 · N370FE · Doug MD1010F · Fuel Control/Turbine Engines
  > STARTED T/O ROLL NR 2 THROTTLE WAS SLOW TO ACHIEVE TAKEOFF POWER. AFTER ACHIEVING TAKEOFF POWER NR 2, N1 ROLLED BACK TO 10 O'CLOCK ON THE GAUGE AND ENGINE FAIL CAME ON AROUND 90 KTS. REMOVED AND REPLACED NR 2 ENGINE VSV FEEDBACK CABLE PER MM 75-31-01-2. REM
- [SDR FDEA201011204432](https://openairdocs.org/sdr/FDEA201011204432.md): Mec · failed · Nov 20, 2010 · N370FE · Doug MD1010F · Fuel Controlling System
  > ON TAKEOFF, NR 2 ENGINE DID NOT REACH T/O, N1 WITH THROTTLE ALIGNED WITH NR1 AND NR3. THROTTLE WAS MOVED SLIGHTLY FWD MANUALLY, AND N1 ROLLED BACK. ENGINE FAIL LIGHT ILLUMINATED, TAKEOFF REJECTED AT 85KTS. INSTALLED FUEL PUMP/MEC IAW MM 73-20-01-2. PERFOME
- [SDR FDEA201010254166](https://openairdocs.org/sdr/FDEA201010254166.md): Floor Panel · punctured · Oct 25, 2010 · N370FE · Doug MD1010F · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL LT SIDE AT STA 1841 IS PUNCTURED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ25-005, REV "H" AND DWG SRZ 25-011, REV "C". REMOVED AND RE-INSTALLED FLOOR PANEL IAW SRM 51- 31-01, VOL II.
- [SDR FDEA201010214165](https://openairdocs.org/sdr/FDEA201010214165.md): Channel · corroded · Oct 21, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CTR CARGO COMPARTMENT AT BS 1521, LBL 56, CHANNEL IS CORRODED. FABRICATED REPAIR ANGLES IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED "J" CHANNEL IAW DAC DWG 2929469. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL II. INSTALLED REPAIR PARTS IAW SRM
- [SDR FDEA201010134043](https://openairdocs.org/sdr/FDEA201010134043.md): Floor Panel · cracked · Oct 13, 2010 · N370FE · Doug MD1010F · Fuselage Floor Panel
  > FWD CARGO PIT FLOOR PANEL 127 UF IS CRACKED. (BS. 791 - 2ND INBD) FABRICATED FLOOR PANEL 127 UF IAW SRZ 25-005, REV H. INSTALLED FLOOR PANEL 127 UF IAW SRM 51-31-01, VOL II.
- [SDR FDEA201010124016](https://openairdocs.org/sdr/FDEA201010124016.md): Skin · dented · Oct 12, 2010 · N370FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RT EXTERIOR FUSELAGE SKIN PRIMARY STATIC PORT CONTROLLED AREA HAS 5 EA DENTS. REPAIRED RT PRIMARY STATIC PORT CONTROLLED AREA DENTS, 5 EACH IAW EA 8-5330-123564, REV "IR" 10-1-10, ALL DENTS FOUND TO BE WITHIN LIMITS EA 8-5330-123564, REV "IR" 10-1- 10, AND
- [SDR FDEA201010073970](https://openairdocs.org/sdr/FDEA201010073970.md): Intercostal · corroded · Oct 7, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPARTMENT BILGE AREA INTERCOSTAL IS CORRODED AT BS 1724; RBL 3. REMOVED ROLLER TRAY TO F.O.M. IAW MD/DC10 SRM 51-31-01, VOL II. REMOVED VHF ANTENNA TO F.O.M. REMOVED INTERCOSTAL TO F.O.M. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. OR
- [SDR FDEA201010073969](https://openairdocs.org/sdr/FDEA201010073969.md): Tube · cracked · Oct 7, 2010 · N370FE · Doug MD1010F · Engine Thrust Reverser
  > NR1 ENG LT THRUST REVERSER GREEN COOLING TUBE IS CRACKED. R & R NR1 ENG LT THRUST REVERSER COOLING TUBE IAW AMM70-00-00; AMM 78-32-14; 70-32-01; SRM 51-21-01 AND SRM 51-41-01.
- [SDR FDEA201010013853](https://openairdocs.org/sdr/FDEA201010013853.md): Floorboard · punctured · Oct 1, 2010 · N370FE · Doug MD1010F · Fuselage Floor Panel
  > AFT PIT FLOOR BOARD 187 HF HAS SEVERAL PUNCTURES. FABRICATED NEW AFT PIT FLOORBOARD 187 HF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".
- [SDR FDEA201010013852](https://openairdocs.org/sdr/FDEA201010013852.md): Floorboard · punctured · Oct 1, 2010 · N370FE · Doug MD1010F · Fuselage Floor Panel
  > AFT PIT FLOORBOARD 187 GF HAS SEVERAL PUNCTURES. FABRICATED NEW AFT PIT FLOORBOARD PANEL 187 GF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".
- [SDR FDEA201009303817](https://openairdocs.org/sdr/FDEA201009303817.md): Longeron · cracked · Sep 30, 2010 · N370FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY LONGERON 52 BETWEEN STA 859 AND STA 755 HAS A CRACKED FASTENER HOLE. FABRICATED NEW LONGERON IAW DWG ADA 3064 AND SRM 51-10-02, FIG 1, VOL III. ALODINED, PRIMED AND PAINTED LONGERON 52 IAW SRM 51-21-01, VOL II. INSTALLED LONGERON 52 IAW SRM 5
- [SDR FDEA201009293793](https://openairdocs.org/sdr/FDEA201009293793.md): Failsafe · corroded · Sep 29, 2010 · N370FE · Doug MD1010F · Fuselage Main, Structure
  > CAC FRAME FAILSAFE ANGLE IS CORRODED STA 1119; LONGERON 51 RT. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1-B, VOL II. REMOVED INTERCOSTALS AT STA 1119 TO 1099; RBL 6 AND LONGERON 51 TO F.O.M. IAW SRM 51-30-0, VOL II. MATERIAL ID FOR REPAIR F
- [SDR FDEA201009293795](https://openairdocs.org/sdr/FDEA201009293795.md): Seat Track · damaged · Sep 29, 2010 · N370FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK SCALLOP IS BROKEN AT BS 775 RBL 8. REMOVED AND RE-INSTALLED FLOOR BOARD PANEL LBL 0 TO RBL 27 AT STA 615 - 775. MATERIAL ID NEW SEAT TRACK 49291150-12000, PO 617966.1. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. VOL I. OK TO PRIME,
- [SDR FDEA201009293784](https://openairdocs.org/sdr/FDEA201009293784.md): Floor Panel · debonded · Sep 29, 2010 · N370FE · Doug MD1010F · Fuselage Floor Panel
  > CTR ACCESSORY COMPARTMENT LT STEP IS DEBONDED. REMOVED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW SRM 51-31-01, VOL II. FABRICATED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW DWG SRZ 25-005, REV "H". INSTALLED NEW PANEL IAW SRM 51-31-01, VOL II.
- [SDR FDEA201009293792](https://openairdocs.org/sdr/FDEA201009293792.md): Skin · gouged · Sep 29, 2010 · N370FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR CUTOUT, AFT SKIN DOUBLER AT APPROXIMATELY STA 999; STRINGER 40 IS GOUGED AND MISSING MATERIAL. REMOVED DOUBLER IAW MD/DC10 SRM 51-31-01, VOL II. GENERATED RFTS N370FE-28-43009 MATERIAL ID TO FABRICATED A NEW DOUBLER IS 2024-T3 0.125, PO 674
- [SDR FDEA201009233778](https://openairdocs.org/sdr/FDEA201009233778.md): Wedge · corroded · Sep 23, 2010 · N370FE · Doug MD1010F · Trailing Edge Flaps
  > RT OTBD FLAP SEC WEDGE PANEL, INBD TOP SKIN REQUIRES REPLACEMENT BECAUSE OF CORROSION. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II. FABRICATED 1 EA DOUBLER IAW DWG ARC 1953, REV "J". FABRICATED -34 AND -35 TEE CAPS IAW DWG ARC 1953
- [SDR FDEA201009233689](https://openairdocs.org/sdr/FDEA201009233689.md): Gusset · cracked · Sep 23, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CABIN INTERNAL FRAME GUSSET IS CRACKED BETWEEN BS 1480 AND BS 1482, STRINGER 16R - STRINGER 17R. FABRICATED NEW CHANNEL IAW DWG 88277. HEAT TREATED CHANNEL FROM 7075-0 TO 7075-T6 PER DWG AWE 7017, REV "AH" AND IAW DPS 7.0. LOCATED AND DRILLED NEW CHA

Next page: https://openairdocs.org/deregistered/N370FE-2018-05-09/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 = 'N370FE' AND deregistration_id = 'N370FE-2018-05-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N370FE-2018-05-09/reports

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