# Service difficulty reports: N375FE, cancelled Mar 2, 2024

A list on [N375FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N375FE-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 · 127 reports

- [SDR FDEA2023012312917](https://openairdocs.org/sdr/FDEA2023012312917.md): Cable · frayed · Nov 10, 2019 · N375FE · Doug MD1010F · Passenger/Crew Doors
  > REISSUED PREVIOUS MEL, REF 52-10-9523. L1 DOOR CABLE. MEL 10NOV19 18:20 MEM U RELEASED FOR SERVICE PER MEL: 52-10-02-01 CATEGORY: C EXPIRATION: 20NOV19 "MEL 52-10-02-01: C/7207131 REMOVED AND REPLACED L1 CABIN DOOR LOWER FWD DRIVE CABLE IA
- [SDR FDEA201908091822](https://openairdocs.org/sdr/FDEA201908091822.md): Wire Harness · failed · Aug 9, 2019 · N375FE · Doug MD1010F · Engine Indicating System Wiring
  > PASSING 12000 AT 302 KTS WITH CLIMB POWER SELECTED. NR 2 ENGINE EGT ROSE QUICKLY TO 1077 DEGREE, THEN FLUCTUATED FOR 2 SECONDS. PULLED THROTTLE TO IDLE AND EGT RETURED TO NORMAL PARAMETERS. ALL OTHER NR 2 ENGINE INDICATIONS NORMAL THROUGHT EVENT. REMOVED
- [SDR FDEA2019080211783](https://openairdocs.org/sdr/FDEA2019080211783.md): Coalescer Bag · odor · Aug 1, 2019 · N375FE · Doug MD1010F · Humidity Control System
  > ELECTRICAL SMELLING SMOKE IMMNATED FROM CAPTAIN SIDE OF COCKPIT @ CRUISE LEVEL 360. SMOKE LASTED APPROX 2-3 MINUTES AND THEN DISIPATED. PERFORMED DUCT CLEANING PROCEDURES, REF MD10 MM 21-53-00-7. REMOVED 3 COALESCER BAGS, RAN THREE ENGINES. RAN THREE
- [SDR FDEA2019041640792](https://openairdocs.org/sdr/FDEA2019041640792.md): Battery · inoperative · Apr 14, 2019 · N375FE · Doug MD1010F · Life Raft
  > DURING PRE FLIGHT LEFT SIDE RAFT LIGHT DID NOT TEST. REPLACED THE BATTERIES.
- [SDR FDEA201902150420](https://openairdocs.org/sdr/FDEA201902150420.md): Cylinder · failed · Feb 15, 2019 · N375FE · Doug MD1010F · Landing Gear Retraction/Extension System
  > AFTER T/O, RECEIVED LT LG MAIN GEAR UNSAFE INDICATION ON PRIMARY AND SECONDARY GEAR RETRACTION GEAR INDICATION. RAN QRH, GEAR PRIMARY OR SECONDARY LIGHTS ILLUMINATED W/ GEAR HANDLE UP CHECKLIST. LT MAIN GEAR UNSAFE INDICATION REMAINED ILLUMINATED. DUMPED APPRO
- [SDR FDEA201902070265](https://openairdocs.org/sdr/FDEA201902070265.md): Sensor · out of alignment · Feb 7, 2019 · N375FE · Doug MD1010F · Landing Gear Position and Warning
  > PDIS 375 32-60 8663 06FEB19 LAX FACT U LOGPAGES:3071618 AFTER T/O, L MAIN GEAR UNSAFE UP. RAN QRH. STILL UNSAFE. SHGN 06FEB19 21:39 LAX U SWUNG GEAR 20 TIMES, UNABLE TO DUPLICATE FAULT. A/C ON JACKS, NEEDS FURTHER TROUBLESHOOTING. FACT 0
- [SDR FDEA201808172070](https://openairdocs.org/sdr/FDEA201808172070.md): Skin · gouged · Aug 17, 2018 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN GOUGED, COVERED BY THE RR BODY FAIRING, AT THE MID SECTION. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIG 6, VOL 1, 53-00-01, FIG.1A, HFEC IAW NTSPM 06-10-01-001. MAJOR REPAIR.
- [SDR FDEA2018081412010](https://openairdocs.org/sdr/FDEA2018081412010.md): Hinge · worn · Aug 11, 2018 · N375FE · Doug MD1010F · Fuselage, Door Hinge
  > CENTER CARGO DOOR FWD HINGE LOBE DIAMETER, FUSELAGE SIDE, EXCEEDED ITS WEAR LIMITS. REMOVED AND REPLACED CENTER CARGO DOOR FWD HINGE IAW AMM 52-32-04-2, AND SRM 51-31-01. OPS CHECK ACCOMPLISHED ON 52T3906. MAJOR REPAIR
- [SDR FDEA201804070927](https://openairdocs.org/sdr/FDEA201804070927.md): Switch · failed · Apr 7, 2018 · N375FE · Doug MD1010F · Emergency Equipment
  > DURING PREFLIGHT OF PUSH TO TEST SWITCH FOR THE R1 DOOR, THE SWITCH BROKE INTO PIECES.
- [SDR FDEA201803220759](https://openairdocs.org/sdr/FDEA201803220759.md): Coalescer Bag · dirty · Mar 22, 2018 · N375FE · Doug MD1010F · Humidity Control System
  > DURING DESCENT THRU 13000 FT, FUMES FROM PACKS WERE EXCESSIVE. FOLLOWED QRH, NR 1 & 2 PACKS WERE ON. FIRST OFFICER DETECTED A MUSTY ODOR. REMOVED AND REPLACED DIRTY 1, 2, & 3 ACM COALESCER BAGS IAW AMM 21-54-03. INSPECTED PACKS FOR CONTAMINATION, NONE NOTED.
- [SDR FDEA201710243035](https://openairdocs.org/sdr/FDEA201710243035.md): Pump · malfunctioned · Oct 24, 2017 · N375FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > NR 2 ENGINE WOULD NOT ACHIEVE CLIMB POWER. THE THROTTLE WAS FIRE WALLED DURING CLIMB, ALL INDICATIONS CONSISTANTLY LESS THAN 1 & 3. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-12-01-2. REMOVED AND REPLACED MEC IAW AMM 73-20-01-2. PREFORMED
- [SDR FDEA201708012091](https://openairdocs.org/sdr/FDEA201708012091.md): Slide · failed · Aug 1, 2017 · N375FE · Doug MD1010F · Escape Slide
  > WHILE TRYING TO PUT NEW ARD ON ACFT, FOUND L1 DOOR ARMED WENT THRU L2 DOOR AND AFTER TRYING TO RESET L1 DOOR BOTTLE BLEW AND SLIDE FELL OUT OF RETAINER CASE. REMOVED AND REPLACED THE L1 DOOR EVACUATION SLIDE CONTAINER IAW MM 25-61-01-2. OK FOR SERVICE
- [SDR FDEA201705061362](https://openairdocs.org/sdr/FDEA201705061362.md): Bottle · low pressure · May 6, 2017 · N375FE · Doug MD1010F · Service Doors
  > R1 DOOR PNEUMATIC ASSIST BOTTLE HAS NO PRESSUE. REMOVED AND REPLACED THE DOOR ASSIST BOTTLE IAW MM 52-11-07-2. OPS CHECKED GOOD IAW AMM 52-10-01-2.
- [SDR FDEA201606172036](https://openairdocs.org/sdr/FDEA201606172036.md): Skin · cracked · Jun 17, 2016 · N375FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING, AT THE INBD SLAT AREA, L/E OF WING, THE NR 1 SLAT TRACK CUTOUT IS CRACKED AT THE LOWER INBD CORNER, THE CRACK IS APPROXIMATELY 1" LONG THE CRACK IS NEAR A PREVIOUS REPAIR. REMOVED OLD DOUBLER, FABED A NEW DOUBLER TO INCORPATE THE OLDER DAMAGE IN WI
- [SDR FDEA201606152016](https://openairdocs.org/sdr/FDEA201606152016.md): Floor Panel · punctured · Jun 15, 2016 · N375FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD BETWEEN STA 600-670 AND FROM LBL 75.5-LBL102 HAS PUNCTURE ABOARD, SEVERAL INSERTS DAMAGED. FABRICATED FLOOR PANEL ON T16/1211640. REMOVAL AND INSTALLATION IS COVERED ON RIM, FIT CARDS.
- [SDR FDEA201507102190](https://openairdocs.org/sdr/FDEA201507102190.md): Cowling · abnormal · Jul 10, 2015 · N375FE · Doug MD1010F · Engine Cowling System
  > AIRCRAFT ARRIVED WITH NR 2 ENG LT FAN COWL MISSING. PERFORMED GVI OF FAN COWL ATTACH POINTS, APPEARS THAT FAN COWL HINGES SEPARATED FROM PYLON STRUCTURE WITH COWLING. UNABLE TO GET A DETAILED CLOSER LOOK AT THIS TIME. ADDING PICTURES TO THE DISCREPANCY. REP
- [SDR FDEA201507082172](https://openairdocs.org/sdr/FDEA201507082172.md): Cowl Door · missing · Jul 8, 2015 · N375FE · Doug MD1010F · Engine Cowling System
  > AIRCRAFT ARRIVED WITH NR 2 ENG LT FAN COWL MISSING. PERFORMED GVI OF FAN COWL ATTACH POINTS, APPEARS THAT FAN COWL HINGES SEPARATED FROM PYLON STRUCTURE WITH COWLING. UNABLE TO GET A DETAILED CLOSER LOOK AT THIS TIME. ADDING PICTURES TO THE DISCREPANCY. DAM
- [SDR FDEA201505101459](https://openairdocs.org/sdr/FDEA201505101459.md): Cylinder · leaking · May 10, 2015 · N375FE · Doug MD1010F · Steering Unit
  > AFTER TAKEOFF LEVEL 2 ALERT HYD 1 FAIL FLUID GONE IAW AMM 32-52-01-2-0. UPON ARRIVAL INTO GATE FOUND LT NOSE WHEEL STEERING CYLINDER LEAKING HYD FLUID. R & R LT NOSE WHEEL STEERING CYLINDER IAW AMM 32-52-01-2. LEAK CHECK & OPERATIONS CHECK GOOD IAW WRI 29-1
- [SDR FDEA201504021136](https://openairdocs.org/sdr/FDEA201504021136.md): Light · inoperative · Apr 2, 2015 · N375FE · Doug MD1010F · Door Warning System
  > LIGHT INDICATING L1 ENTRY DOOR IS DISARMED & DOES NOT ILLUMINATE WHEN THE DOOR IS DISARMED. RELAMPED L1 ENTRY DOOR, DISARMED LIGHT ASSEMBLY. LIGHT OPERATIONS CHECKED GOOD IAW AMM: 52-11-00.
- [SDR FDEA201411173720](https://openairdocs.org/sdr/FDEA201411173720.md): Pressure Switch · failed · Nov 17, 2014 · N375FE · Doug MD1010F · Airfoil Anti/De-ice System
  > WING ANTI-ICE DISAGREE AFTER TAKEOFF, FOLLOWED BY AIR SYS 1 OFF. AFTER CONSULTING MOC & GOC RETURNED. TROUBLESHOOTING IAW FIM 30-11 TASK 801. AIR SYS 1 OFF ALERT SUGGESTS USING FIM 36-23 TASK 803. FOUND FAULT BALL ON PNEUMATIC MANIFOLD FAULT INDICATOR PRE
- [SDR FDEA201409262804](https://openairdocs.org/sdr/FDEA201409262804.md): Switch · inoperative · Sep 26, 2014 · N375FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR ESCAPE SLIDE LOW PRESS INDICATOR PRESS TO TEST LIGHT INOPERATIVE. R & R R1 DOOR PRESS TO TEST SWITCH IAW SWPS. OPERATIONS NOW NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201408022036](https://openairdocs.org/sdr/FDEA201408022036.md): Bulb · failed · Aug 2, 2014 · N375FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST LIGHT NOT ILLUMINATING WHEN PUSHED. REMOVED AND REPLACED BULBS. CHECKED OK IAW AMM 25-61-03-5.
- [SDR FDEA201405130991](https://openairdocs.org/sdr/FDEA201405130991.md): Warning System · false activation · May 13, 2014 · N375FE · Doug MD1010F · Landing Gear Position and Warning
  > ON FINAL GOT NO GEAR DOWN & LOCKED INDICATIONS ON HANDLE OR EAD SYNOPTIC, LIGHTS ALL RED, WENT AROUND, RAN QRH GEAR LIGHTS ALL GREEN AFTER QRH. SUSPECT SWITCH INDICATOR AS MULTIPLE WRITE UPS. FAILED OPERATIONS CHECK & ORIGINAL UNIT REINSTALLED. TROUBLE SHOT
- [SDR FDEA201404290888](https://openairdocs.org/sdr/FDEA201404290888.md): Bushing · missing · Apr 29, 2014 · N375FE · Doug MD1010F · Landing Gear Position and Warning
  > LT MLG UNSAFE AFTER TO. FLASHED ON & OFF DURING QRH CHECKLIST. REVIEWED PSEU CURRENT FAULTS, NONE REPORTED IN FAULT REVIEW. REPORTS OF LT GEAR UP & LATCHED, AB SENSOR DISAGREE. VERIFIED CLEARANCE BETWEEN SENSOR & TARGET, FOUND THE ATTACH BOLT FOR THE LINK
- [SDR FDEA201404290887](https://openairdocs.org/sdr/FDEA201404290887.md): Warning System · false activation · Apr 29, 2014 · N375FE · Doug MD1010F · Landing Gear Position and Warning
  > LEFT MAIN GEAR RED LIGHT STAYED ON AFTER RETRACTION. COMPLIED WITH QRH & LIGHT WENT OUT ON SECOND TRY. TROUBLE SHOT IAW FIM 32-30-01. INSPECTED LT MLG HYD COMPONENTS & FOUND NO LEAKS OR OTHER DISCREPANCIES. PERFORMED BITE CHECK OF PSEU & FOUND NO CURRENT F
- [SDR FDEA201402080288](https://openairdocs.org/sdr/FDEA201402080288.md): Aiu · failed · Feb 8, 2014 · N375FE · Doug MD1010F · Pneumatic Distribution System
  > RECEIVED A LEVEL ON, AIR SYS 2 OFF ALERT, FOLLOWED BY A LEVEL 3 AIR MANIFOLD 2 FAIL ALERT IN FLIGHT. RED MANIFOLD LIGHT FOR BLEED AIR 2. IAW QRH, THROTTLE IDLE, TEMP IN MANIFOLD 2 DECREASED. R & R NR 2 AIU IAW AMM 31-43-02-4. OPS CHECKED IAW AMM 31-43-0
- [SDR FDEA201312183002](https://openairdocs.org/sdr/FDEA201312183002.md): Unknown · malfunctioned · Dec 18, 2013 · N375FE · Doug MD1010F · Stabilizer Control System
  > REJECTED TAKEOFF DUE TO CAWS, STABILIZER MOTION, ALERT AT ABOUT 100KTS NOTICED STAB TRIM WAS 0.2 UNITS, GREATER THAN BEFORE TAKEOFF SETTING. ON SUBSEQUENT TAKEOFF NO CAWS. HOWEVER JUST PRIOR TO ROTATION, FIRST OFFICER NOTED THAT STAB TRIM HAD DECREASED BY 0.
- [SDR FDEA201311162796](https://openairdocs.org/sdr/FDEA201311162796.md): Target · contaminated · Nov 16, 2013 · N375FE · Doug MD1010F · Landing Gear Position and Warning
  > LEFT MAIN GEAR UNSAFE ON RETRACTION. BOTH PRIMARY AND SEC. INDICATIONS UNSAFE WITH GEAR HANDLE UP, CYCLED GEAR IAW QRH. 3 SAFE INDICATIONS BOTH PRI AND SEC. ACCESSED PSEU THROUGH CFDS. FOUND FAULT CODE 317067 "PSEU NO CFDS DATA". TROUBLESHOT IAW MD10 FIM 3
- [SDR FDEA201210013518](https://openairdocs.org/sdr/FDEA201210013518.md): Proximity Sensor · dirty · Oct 1, 2012 · N375FE · Doug MD1010F · Landing Gear Position and Warning
  > AFTER TAKE OFF, RAISED GEAR. LT MAIN HAD PRIMARY AND SECONDARY UNSAFE INDICATION. COMPLIED WITH QRH PROCEDURE AND CYCLED GEAR. NOW PRIMARY AND SECONDARY INDICATIONS UP AND LOCKED. LT GEAR UP AND LATCHED A/B SENSOR DISAGREE FAULT. CHECKED RTS ON PSEU BOX AN
- [SDR FDEA201206042073](https://openairdocs.org/sdr/FDEA201206042073.md): Blade · damaged · Jun 4, 2012 · N375FE · Doug MD1010F · Turbine Engine Compressor Section
  > ON POST FLIGHT, FOUND FOD DAMAGE TO NR 3 ENGINE FAN BLADE WITH BIRD REMAINS VISIBLE. PERFORMED FOD BOROSCOPE INSPECTION IAW MD10 AMM 72-00-00-6-1, FIG 609, ITEMS 5 AND 10 WITH NO LIMITING DEFECTS FOUND. PERFORMED FOD CLOSED COWLING INSPECTION IAW AMM 72-00-0
- [SDR FDEA201205161815](https://openairdocs.org/sdr/FDEA201205161815.md): Shear Tie · damaged · May 16, 2012 · N375FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT LOWER FUSELAGE AT STA 1801 L-51L HAS RIVET HEAD SHEARED. REMOVED FASTENERS AND DAMAGED SHEAR TIE IAW SRM 51-31-01. FABRICATED SHEAR TIE. TREATED, PRIMED AND TOPCOATED IAW SRM 53-30-00, SRM 51-21-01 AND SRM 51-21-02. INSTALLED SHEAR TIE IAW SRM 53-30-00
- [SDR FDEA201205111798](https://openairdocs.org/sdr/FDEA201205111798.md): Skin · gouged · May 11, 2012 · N375FE · Doug MD1010F · Trailing Edge Flaps
  > GOUGES IN RT OTBD FLAP LOWER SKIN WS 500 CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01, L=1.0" X W=.50" X D=.085". FABRICATED DOUBLER IAW SRM 57-10-00. INSTALLED DOUBLER IAW SRM 51-31-01.
- [SDR FDEA201205101786](https://openairdocs.org/sdr/FDEA201205101786.md): Seat Track · damaged · May 10, 2012 · N375FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK STA 1381, LBL 75 FOUND TO HAVE BROKEN EARS. REMOVED DAMAGED SEAT TRACK SECTION BS 1371 TO 1409. FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-70-00, FIG 1 AND SRM 51-31-01.
- [SDR FDEA201104171508](https://openairdocs.org/sdr/FDEA201104171508.md): Lamp · inoperative · Apr 17, 2011 · N375FE · Doug MD1010F · Instrument Panel
  > BOTH EMERGENCY POWER "OFF" AND "ON" LIGHTS INOPERATIVE REGARDLESS OFF BATTERY SWITCH POSITION. RELAMPED AFFECTED SWITCH LIGHTS IAW AMM 33-11-17-2-0. ALL OPS CHECKS NORMAL.
- [SDR FDEA201104011277](https://openairdocs.org/sdr/FDEA201104011277.md): Handle · out of sequence · Apr 1, 2011 · N375FE · Doug MD1010F · Passenger/Crew Doors
  > DURING PREFLIGHT COULD NOT OPERATE DOOR R1, FOUND THE EMERGENCY BOTTLE HANDLE OUT OF SEQUENCE MEL 01APR11, 03:10 IAD R RELEASED FOR SERVICE IAW MEL: 52-10-03 CATEGORY: C EXPIRATION: 11APR11 "MEL 52-10-03: (IDENTIFY L1 OR R1) R1 MAIN ENTRY (IDENTIFY DOOR OR
- [SDR FDEA201103030834](https://openairdocs.org/sdr/FDEA201103030834.md): Web · cracked · Mar 3, 2011 · N375FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CTR WHEEL RT SIDE WALL, BETWEEN THE SECOND AND THIRD STATIONS AFT OF THE FWD BULKHEAD APPROX STA 1381 TO 1401. THERE ARE 9 CRACKS IN A DOUBLER. REMOVED AND REPLACED BARREL KEEL SPLICE DOUBLER. REF SRM 51-33-01 VOL 2 AND E.A. 8-5310-149330 AND E.A. 8-5310-148
- [SDR FDEA201103030832](https://openairdocs.org/sdr/FDEA201103030832.md): Bulkhead · cracked · Mar 3, 2011 · N375FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CTR WHEEL WELL, RT SIDE WALL, BETWEEN STA 1381 AND 1401 LIGHTNING HOLE NEAR TOP HAS A CRACK COMING OUT OF IT. VERIFIED BY HFEC REPAIRED CTR WHEEL WELL RT SIDE WALL AT APPROX 1381 AND 1401, REF EA 8-5310-148492 AND EA 8-5310-149330.
- [SDR FDEA201007272681](https://openairdocs.org/sdr/FDEA201007272681.md): Skin · misrepaired · Jul 27, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 1979 TO STA 2007 BETWEEN LONGERON 48R AND LONGERON 47L. EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 1979 TO STA 2007 BETWEEN LONGERON 48R AND LONGERON 47L EVALUATED AND FOUND NOT CONFORM TO SRM. EXISTING REPAIR R &
- [SDR FDEA201007272680](https://openairdocs.org/sdr/FDEA201007272680.md): Bulkhead · misrepaired · Jul 27, 2010 · N375FE · Doug MD1010F · Fuselage Main, Bulkhead
  > EXISTING REPAIR AT FWD CARGO PRESSURE BULKHEAD STA 595 BETWEEN LONGERON 42R AND LONGERON 43R. EXISTING REPAIR AT FWD CARGO PRESSURE BULKHEAD STA 595 BETWEEN LONGERON 42R AND LONGERON 43R EVALUATED AND FOUND NOT IAW SRM REPAIR. EXISTING REPAIR REMOVED AND NEW
- [SDR FDEA201007272674](https://openairdocs.org/sdr/FDEA201007272674.md): Skin · misrepaired · Jul 27, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 2007 TO STA 2014 LONGERON 50R. EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. SKIN REPLACEMENT CARRIED OUT IAW DWG AJC7207 REV FK AND SRM 51-31-01 VOLUME II, REV 96. EO 8-5100-7-5001, A7, PART 1, REPAIR CLASSIF
- [SDR FDEA201007272679](https://openairdocs.org/sdr/FDEA201007272679.md): Skin · dented · Jul 27, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE STA 495, BETWEEN LONGERON 25R TO LONGERON 27R, SKIN FOUND WITH DENT AND AN ELONGATED HOLE AFTER EXISTING TEMPORARY REPAIR DOUBLERS REMOVED. FUSELAGE STA 495, BETWEEN LONGERON 25R TO LONGERON 27R, SKIN REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6 (SHEET
- [SDR FDEA201007262669](https://openairdocs.org/sdr/FDEA201007262669.md): Skin · misrepaired · Jul 26, 2010 · N375FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > EXISTING FLUSH REPAIR AT RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN XFS 289. EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT AS PER E.A. 8-5510-132438. E.O. 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA201007262672](https://openairdocs.org/sdr/FDEA201007262672.md): Skin · misrepaired · Jul 26, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT LOWER FUSELAGE SKIN INTERNAL DOUBLER STA 859 L-31R. EXISTING REPAIR AT LOWER FUSELAGE SKIN INTERNAL DOUBLER STA 859 L31R EVALUATED AND FOUND NOT IAW SRM REPAIR. EXISTING REPAIR R & R WITH NEW REPAIR IAW EA 8-5330-138581 TITLE: MAINFRAMES -
- [SDR FDEA201007262668](https://openairdocs.org/sdr/FDEA201007262668.md): Floorbeam · misrepaired · Jul 26, 2010 · N375FE · Doug MD1010F · Fuselage Main, Floor Beam
  > EXISTING REPAIR AT FORWARD CARGO FLOORBEAM STATION 979. EXISTING REPAIR AT FORWARD CARGO FLOORBEAM STATION 979 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT INACCORDANCE WITH SRM REPAIR SCHEME. EXISTINGREPAIR REMOVED AND REPLACED WITH NEW REPAIR AS PER E.A.
- [SDR FDEA201007262667](https://openairdocs.org/sdr/FDEA201007262667.md): Frame · misrepaired · Jul 26, 2010 · N375FE · Doug MD1010F · Fuselage Main, Frame
  > EXISTING REPAIR AT WASTE TANK COMPARTMENT FRAME STATION 1986 L-50L TO L-50R. PRVIOUSLY ACCOMPLISHED NOT IAN ACCORDANCE WITH SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND REPLACED WITH NEW REPAIR AS PER SRM 53-30-00 FIG. 5 VOL. 1 REV. 96. EO 8-5100-7-5001 A
- [SDR FDEA201007242662](https://openairdocs.org/sdr/FDEA201007242662.md): Skin · unknown · Jul 24, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT FUSELAGE UPPER SKIN STA 1771 BETWEEN LONGERON 4R TO LONGERON 5R. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED IAW SRM 53-20-00, FIG 6, VOL I, REV 96. EO8-5100-7-5001, A7 P1 TITLE: "STRUCTURES-REPAIR CATALOG - REPAIR IDENTIFICATION
- [SDR FDEA201007242661](https://openairdocs.org/sdr/FDEA201007242661.md): Skin · unknown · Jul 24, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT FUSELAGE SKIN LOWER STA 795 BETWEEN LONGERON 49L AND LONGERON 50L. EXISTING REPAIR REMOVED AND REPLACED AS PER SRM 53-20-00 FIG 6 VOL 1 REV 96 EO 8-5100-7-5001 A7 PT1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.
- [SDR FDEA201007242660](https://openairdocs.org/sdr/FDEA201007242660.md): Skin · misrepaired · Jul 24, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT FUSELAGE ABOVE FWD LOWER CARGO DOOR CONTROL PANEL STA 859. FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND CARRIED OUT REPAIR AS PER E.A. 8-5330-138581. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION
- [SDR FDEA201007242659](https://openairdocs.org/sdr/FDEA201007242659.md): Skin · misrepaired · Jul 24, 2010 · N375FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT FUSELAGE SKIN BELLY STA 919, 6 O'CLOCK POSITION. EVALUATED PREVIOUSLY ACCOMPLISHED NOT IAN ACCORDANCE WITH SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND REPLACED AS PER SRM 53-20-00 FIG. 6 VOL. I REV. 96. E.O. 8-5100-7-5001 A7 PT1. R
- [SDR FDEA201007222643](https://openairdocs.org/sdr/FDEA201007222643.md): Longeron · unknown · Jul 22, 2010 · N375FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > EXISTING REPAIR AT FORWARD CARGO STATION 879 TO STATION 899 LONGERON 50R. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-00-00 FIG 2 VOL I REV 96 EO EO 8-5100-7-5001 A7 PT 2.

Next page: https://openairdocs.org/deregistered/N375FE-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 = 'N375FE' AND deregistration_id = 'N375FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N375FE-2024-03-02/reports

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