# Service difficulty reports: N655FE

A list on [N655FE](https://openairdocs.org/aircraft/N655FE.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 · 219 reports

- [SDR FDEA202510061904](https://openairdocs.org/sdr/FDEA202510061904.md): Bottle · low pressure · Oct 6, 2025 · N655FE · Airbus A300F4605R · Service Doors
  > R1 DOOR EMERGENCY DAMPENER BELOW MIN NITROGEN CHARGE. AMM 52-10-14-03-02 SERVICED R1 DOOR EMERGENCY DAMPENER CYLINDER TO WITHIN LIMITS PER PLACARD AND AMM 52-10-14-03-02 STEP 3.D.(12) OKAY TO CONTINUE.
- [SDR FDEA202409131400](https://openairdocs.org/sdr/FDEA202409131400.md): Rib · corroded · Sep 13, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE UPPER BORE OF INBD JACK RIB(LOCATION#1) WAS CORRODED ON L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA
- [SDR FDEA202409131385](https://openairdocs.org/sdr/FDEA202409131385.md): Rib · corroded · Sep 13, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE UPPER BORE OF INBD JACK RIB(LOCATION#1) WAS CORRODED ON L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA
- [SDR FDEA202409121488](https://openairdocs.org/sdr/FDEA202409121488.md): Rib · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH SPOILER 3 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #3 SPOILER OUTBD JACK RIB UPPER BORE I.A.W FEDEX EA NO: T6-5740-T0380720 P1, SEQ NO:791, TITLE: WINGS- ATTACH FITTINGS- RH WING #3 SPOILER JACK RIB AT STA ABX 40
- [SDR FDEA202409121399](https://openairdocs.org/sdr/FDEA202409121399.md): Rib · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE LWR BORE OF INBD JACK RIB WAS CORRODED ON L5 SPLR(LOCATION #3). ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA A
- [SDR FDEA202409121396](https://openairdocs.org/sdr/FDEA202409121396.md): Rib · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH SPOILER 5 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER OUTBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380713 P1, SEQ NO:789, TITLE: WINGS- ATTACH FITTINGS- RH WING #5 SPOILER JACK RIB AT STA ABX 175.875 AND A
- [SDR FDEA202409121395](https://openairdocs.org/sdr/FDEA202409121395.md): Rib · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH SPOILER 5 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380713 P1, SEQ NO:789, TITLE: WINGS- ATTACH FITTINGS- RH WING #5 SPOILER JACK RIB AT STA ABX 175.875 AND ABX184
- [SDR FDEA202409121394](https://openairdocs.org/sdr/FDEA202409121394.md): Rib · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH SPOILER 3 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #3 SPOILER OUTBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380720 P1, SEQ NO:791, TITLE: WINGS- ATTACH FITTINGS- RH WING #3 SPOILER JACK RIB AT STA ABX 40.425- BEAM
- [SDR FDEA202409121393](https://openairdocs.org/sdr/FDEA202409121393.md): Rib · gouged · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE UPPER BORE OF INBD JACK RIB (LOCATION #1) GOUGE ON L4 SPOILER ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #4 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380723 P1, SEQ NO:792, TITLE: WINGS- ATTACH FITTINGS- LH WING #4 SPOILER JACK RIB AT STA ABX
- [SDR FDEA202409121392](https://openairdocs.org/sdr/FDEA202409121392.md): Rib · gouged · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE UPPER BORE OF INBD JACK RIB (LOCATION #1) GOUGE ON L4 SPOILER ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #4 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380723 P1, SEQ NO:792, TITLE: WINGS- ATTACH FITTINGS- LH WING #4 SPOILER JACK RIB AT STA ABX
- [SDR FDEA202409121386](https://openairdocs.org/sdr/FDEA202409121386.md): Rib · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE LWR BORE OF INBD JACK RIB WAS CORRODED ON L5 SPLR(LOCATION #3). ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA A
- [SDR FDEA202409121370](https://openairdocs.org/sdr/FDEA202409121370.md): Seat Track · corroded · Sep 12, 2024 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK A POINT GOT CORROSION AT FR15B Y953 REPLACED THE SEAT TRACK WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100. AT FR15A~19, Y953
- [SDR FDEA202409121332](https://openairdocs.org/sdr/FDEA202409121332.md): Seat Track · corroded · Sep 12, 2024 · N655FE · Airbus A310300 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK A POINT GOT CORROSION AT FR15B Y953 REPLACED THE SEAT TRACK WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100. AT FR15A~19, Y953 NOTE: 5.(C), P/N TYPE ERROR, CREATED A NEW SDR NO:24-
- [SDR FDEA202409111407](https://openairdocs.org/sdr/FDEA202409111407.md): Fitting · cracked · Sep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > LOWER RH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE DOUBLER REPAIR AT FRAME FOOT FR 46, STGR36R~38R. I.A.W FEDEX EO NO:E6-5310-E0330747 D P26, SEQ NO:784, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 A
- [SDR FDEA202409111406](https://openairdocs.org/sdr/FDEA202409111406.md): Fitting · cracked · Sep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > LOWER LH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE DOUBLER REPAIR AT FRAME FOOT FR 46, STGR36L~38L. I.A.W FEDEX EO NO:E6-5310-E0330747 D P25, SEQ NO:783, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 A
- [SDR FDEA202409111405](https://openairdocs.org/sdr/FDEA202409111405.md): Fitting · cracked · Sep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > LOWER LH FRAME 45 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE DOUBLER REPAIR AT FRAME FOOT FR 45, STGR36L~38L. I.A.W FEDEX EO NO:E6-5310-E0330747 D P23, SEQ NO:782, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 A
- [SDR FDEA202409111404](https://openairdocs.org/sdr/FDEA202409111404.md): Fitting · cracked · Sep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Structure
  > LOWER RH FRAME 44 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE TRIMMED OUT AND FILLED THE GAP UNDER THE ANGLE WITH SHIM AT FR 44, STGR36R~37R I.A.W FEDEX EO NO:E6-5310-E0330747 D P22, SEQ NO: 781, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME B
- [SDR FDEA202403020227](https://openairdocs.org/sdr/FDEA202403020227.md): Slide · detached · Mar 2, 2024 · N655FE · Airbus A300F4605R · Escape Slide
  > R1 DOOR ESCAPED SLIDE FELL OUT OF DOOR WHEN DOOR WAS OPENED. DOOR DID NOT BLOW WHEN IT FELL OUT. REPLACED SLIDE IAW AMM 25-61-21-4.
- [SDR FDEA202206161441](https://openairdocs.org/sdr/FDEA202206161441.md): None · unknown · Jun 16, 2022 · N655FE · Airbus A300* · Brake
  > MDIS 655 32-42 4886 16JUN22 LRD OPEN U # 5 MLG TIRE COMPLETELY MISSING FROM AIRCRAFT AT BLOCK IN. *************************************************** TFOA CATEGORY: 1 SHGN 19JUN22 22:36 LRD
- [SDR FDEA202204181076](https://openairdocs.org/sdr/FDEA202204181076.md): Seat Track · damaged · Apr 18, 2022 · N655FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK COMPT - SEAT TRACK CROWN LIP AREA FOUND ENLARGED AT FR20 6" AND -Y450 CUT OUT AND INSTALLED NEW SEAT TRACK PORTION & REPAIR ANGLES I.A.W EA NO:6-5310- T0367804 P1, SEQ NO:001135, TITLE:FUSELAGE-MAINFRAME- MAIN DECK SEAT TRACKS AT -Y450 & -Y1456 WO
- [SDR FDEA202204181075](https://openairdocs.org/sdr/FDEA202204181075.md): Seat Track · damaged · Apr 18, 2022 · N655FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK COMPT - SEAT TRACK CROWN LIP AREA FOUND ENLARGED AT FR20 6" AND -Y1456 CUT OUT AND INSTALLED NEW SEAT TRACK PORTION & REPAIR ANGLES I.A.W EA NO:6-5310- T0367804 P1, SEQ NO:001135, TITLE:FUSELAGE-MAINFRAME- MAIN DECK SEAT TRACKS AT -Y450 & -Y1456
- [SDR FDEA202203290828](https://openairdocs.org/sdr/FDEA202203290828.md): Floor Panel · none · Mar 29, 2022 · N655FE · Airbus A300* · Fuselage Floor Panel
  > AT THE TIME OF AGING AIRCRAFT INSPECTION FOUND MAIN DECK FLOOR PANEL 242BF IS SHOWING SIGNS OF DELAMINATION REPAIRED WITH RESIN COMPOUND AND FIBER GLASS I.A.W A300-600F SRM 53-10-20-201, PARA.8B, P209-211, FIG203(SHEET 1)
- [SDR FDEA202203210618](https://openairdocs.org/sdr/FDEA202203210618.md): None · worn · Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor Beam
  > FR38.2/FR40 RH NO.2 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202203210617](https://openairdocs.org/sdr/FDEA202203210617.md): None · worn · Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor Beam
  > FR38.2/FR40 CENTER NO.1 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202203210616](https://openairdocs.org/sdr/FDEA202203210616.md): None · worn · Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor Beam
  > FR38.2/FR40 LH NO.2 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202203210615](https://openairdocs.org/sdr/FDEA202203210615.md): None · worn · Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor Beam
  > FR54/FR54.2 LH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202203210614](https://openairdocs.org/sdr/FDEA202203210614.md): None · worn · Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor Beam
  > FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202203200893](https://openairdocs.org/sdr/FDEA202203200893.md): None · unknown · Mar 20, 2022 · N655FE · Airbus A300* · Wing Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTCHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMP) TRK, INSPECTION OF EXISTI
- [SDR FDEA202203200892](https://openairdocs.org/sdr/FDEA202203200892.md): None · none · Mar 20, 2022 · N655FE · Airbus A300* · Wing Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTCHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMP) TRK, INSPECTION OF EXISTI
- [SDR FDEA202203200891](https://openairdocs.org/sdr/FDEA202203200891.md): Seat Track · none · Mar 20, 2022 · N655FE · Airbus A300* · Fuselage Structure (General)
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR OF SPLICE FOUND ON MAIN DECK SEAT TRACK BTW FR67-FR70,Y450 POSITIOS. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPA
- [SDR FDEA202203200671](https://openairdocs.org/sdr/FDEA202203200671.md): Seat Track · corroded · Mar 20, 2022 · N655FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK COMPT FLOOR - SEAT TRACK, FLANGE AREA GOT CORROSION POS FROM FR 55 11" TO FR 56 10" AND Y0. PERFORMED SEAT TRACK SPLICE REPAIR ON CORROSION SECTION I.A.W. A300-600F SRM 53- 10-16-201, PARA.4, PAGE.203-208, FIG.201. "MAJOR REPAIR"
- [SDR FDEA202203180724](https://openairdocs.org/sdr/FDEA202203180724.md): Floor Support · corroded · Mar 18, 2022 · N655FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT GOT CORROSION POS AROUND HARDPOINT AREA FROM FR13 TO FR13A AND Y953 ACCOMPLISHED THE CATE.B FLOOR STRUCTURE REPAIR I.A.W A300-600F SRM 53-12-15-201-2, PARA.5G, PAGE.239-244, FIG.207 & SRI:53-12-15-201, IIR:53-12-15-2-004-00, PARA.
- [SDR FDEA202203150817](https://openairdocs.org/sdr/FDEA202203150817.md): None · worn · Mar 15, 2022 · N655FE · Airbus A300* · Wing, Control Surfaces
  > LH SPL#2 O/B EDGE WEB CHAFING. ACCOMPLISHED THE REPAIR WITH FILLER AND REPAIR SHIM I.A.W EA NO:6-5750-T0367548 P1, SEQ NO:001119, TITLE:WING -FLIGHT SURFACES- LH SPOILER #2 -WEAR MARK ON OUTBOARD FACE OF FRONT SPAR AT LEVEL OF RIB18 & A300-600F SRM 51-27
- [SDR FDEA202203150695](https://openairdocs.org/sdr/FDEA202203150695.md): Plate · cracked · Mar 15, 2022 · N655FE · Airbus A300* · Fuselage Floor Panel
  > AVIONICS COMP'T DOOR AFT EDGE PANEL SUPPORT FRAME CRACK ABOUT0.2". REPLACED THE PLATE BENT WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE2
- [SDR FDEA202203100652](https://openairdocs.org/sdr/FDEA202203100652.md): Floor Panel · damaged · Mar 10, 2022 · N655FE · Airbus A300* · Fuselage Floor Panel
  > THE FWD CARGO FLOOR PANEL #131QG #131LG #131RG #131SG WAS FOUND DAMAGED AS MARKER. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA8B FIG203 SHEET1 P209-211
- [SDR FDEA202203100628](https://openairdocs.org/sdr/FDEA202203100628.md): Skin · damaged · Mar 10, 2022 · N655FE · Airbus A300* · Horizontal Stabilizer Structure
  > 1EA WATER TRAPPED AREA WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL NO.14(130MM X 85MM) SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA CAT.A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA.5J P268-270 FIG 212 (SHEET 3)
- [SDR FDEA202203100627](https://openairdocs.org/sdr/FDEA202203100627.md): Skin · damaged · Mar 10, 2022 · N655FE · Airbus A300* · Horizontal Stabilizer Structure
  > 1EA WATER TRAPPED AREA WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL NO.19(120MM X 80MM) SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA CAT.A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA.5J P268-270 FIG 212 (SHEET 3)
- [SDR FDEA202203100626](https://openairdocs.org/sdr/FDEA202203100626.md): Skin · damaged · Mar 10, 2022 · N655FE · Airbus A300* · Horizontal Stabilizer Structure
  > 1EA WATER TRAPPED AREA WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL NO.20(150MM X 90MM) SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA CAT.A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA.5J P268-270 FIG 212 (SHEET 3)
- [SDR FDEA202111182892](https://openairdocs.org/sdr/FDEA202111182892.md): None · corroded · Nov 18, 2021 · N655FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > AFTER REMOVAL OF THE RH RIB 5, FWD LUG AFT FACE BUSHING, FOUND CORROSION IN BORE AND ON LUG FACE. REPAIRED IAW EA T6-5710-T0365559, PARTS 1, THRU 5. RH RIB 5 FWD LUG BORE & AFT FACE WEAR DAMAGE DUE TO IMPROBERILY INSTALLED MLG BUSHING- SB A300-57-6106
- [SDR FDEA202102230600](https://openairdocs.org/sdr/FDEA202102230600.md): Bulkhead · damaged · Feb 23, 2021 · N655FE · Airbus A300F4605R · Fuselage Main, Structure
  > NLG WHEEL WELL BULKHEAD DAMAGE (STIFFENER CRACK/DEFORMAT COMPLY WITH E..A. 6-5310-T0360151 REV NO. POS. P1 INFO 07MAR21 01:32 ** ATTACHED TO WORK ORDER 00079413 ** STRP 07MAR21 03:12 MEM U FACT 07MAR21 03:12 MEM U COMPLIED WITH EA 6-5310-T0360151
- [SDR FDEA202011032765](https://openairdocs.org/sdr/FDEA202011032765.md): Arming Lever · unknown · Nov 3, 2020 · N655FE · Airbus A300F4605R · Emergency Equipment
  > PDIS 655 52-10 3248 03NOV20 MEM FACT U. UPON CLOSE UP OF A/C 655 THE CABIN ENTRY DOOR ON THE RIGHT SIDE OF THE AIRPLANE WOULD NOT ARM SLIDE. IT ILLUMINATED BRIEFLY, FLASHED ON AND OFF AND THEN STAYED OFF. WE OPENED AND CLOSED DOOR AND ATTEMPTED TO REARM TO
- [SDR FDEA202010232621](https://openairdocs.org/sdr/FDEA202010232621.md): Transmitter · failed · Oct 23, 2020 · N655FE · Airbus A300F4605R · Hydraulic Indicating System
  > PDIS 655 29-30 3219 23OCT20 CLE OPEN U LOGPAGES:3236545 ENROUTE TO CLE AT 350, GOT A ECAM WARNING FOR GREEN HYDRAULIC LO QUANTITY. THE GEEN HYDRAULIC GAUGE SHOWED FLUID BELOW RED DOT. ECAM GAUGE WAS AT THE BOTTOM OF THE SCALE. DIDN'T RECEIVE
- [SDR FDEA202008292065](https://openairdocs.org/sdr/FDEA202008292065.md): Tire · failed · Aug 29, 2020 · N655FE · Airbus A300F4605R · Tire
  > ON APPROACH, GOT A LEFT MAIN DOOR LIGHT. ALL GEAR INDICATIONS WERE ALL GREEN(DOWN AND LOCKED) ADHERED TO QRH. ON LANDING ROLLOUT, HAD AN APPARENT BLOWN TIRE. COMPLIED WITH EA 6-3212-T0356228 REV A PART 2. GEAR SWING TEST GOOD, REF AMM 32-31-00-5 LANDING G
- [SDR FDEA2019120193152](https://openairdocs.org/sdr/FDEA2019120193152.md): Adapter · damaged · Nov 19, 2019 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > RESTRAINT ID C1509 IS UNABLE TO PROVIDE RESTRAINT DUE TO SEAT TRACK DAMAGE. REMOVED AND REPLACED DAMAGED ADAPTER REF SRM 51-40-20 AND SRM 30-53-003. RE-INSTALLED LATCH/RESTRAINT IN 8L.
- [SDR FDEA2019120183153](https://openairdocs.org/sdr/FDEA2019120183153.md): Adapter · damaged · Nov 8, 2019 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ADAPTER ON MAIN CARGO DECK AT POSITION C1509 HAS A BROKEN LOBE. REMOVED AND REPLACED DAMAGED ADAPTER REF SRM 51-40-20 AND SR30-53-003.
- [SDR FDEA201910312796](https://openairdocs.org/sdr/FDEA201910312796.md): Actuator · malfunctioned · Oct 31, 2019 · N655FE · Airbus A300F4605R · Leading Edge Slat Actuator
  > PDIS 655 27-80 2283 30OCT19 FSD OPEN U LOGPAGES:2284251 ON APPROACH FSD - NO KRUGER FLAP EXTENTION - RUN ECAM - QRH - NORMAL LANDING. SHGN 31OCT19 12:53 FSD U FOUND LEFT KRUGER FLAP WITH MOVEABLE VANE ABOVE FLAP. COMPLIED WITH EA. 6-2780
- [SDR FDEA201909052104](https://openairdocs.org/sdr/FDEA201909052104.md): Skin · corroded · Sep 5, 2019 · N655FE · Airbus A300F4605R · Trailing Edge Flaps
  > FROM INSIDE TO OUTSIDE NR 1 STATIC DISCHARGER RETAINER AND SKIN SEPARATION ON THE RT WING TRAILING EDGE. COMPLIED WITH EA:6-5750-T0349278 P1 REPAIRED FROM INSIDE TO OUTSIDE NR 1 STATIC DISCHARGER RETAINER AND SKIN SEPARATION ON THE RT WING TRAILING EDGE. EA TI
- [SDR FDEA201908302041](https://openairdocs.org/sdr/FDEA201908302041.md): Support Beam · cracked · Aug 30, 2019 · N655FE · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SUPPORT BEAM FOUND CRACKED FR61 TO FRAMES 62 TO 62. REPLACED AFT CARGO DOOR SUPPORT BEAM IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201908262017](https://openairdocs.org/sdr/FDEA201908262017.md): Floorbeam · cracked · Aug 26, 2019 · N655FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT DOOR CUTOUT AREA, FLOOR BEAM ABOUT FRAME 60 FOUND CRACKED. COMPLIED WITH EA:6-5310-T0348991 P1, REPAIRED AFT CARGO COMPARTMENT DOOR CUTOUT AREA, FLOORBEAM ABOUT FRAME 60. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201908221998](https://openairdocs.org/sdr/FDEA201908221998.md): Crossbeam · cracked · Aug 22, 2019 · N655FE · Airbus A300F4605R · Fuselage Main, Structure
  > CROSSBEAM ON NLG FR15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACKED. COMPLIED WITH EA 6-5310-T0348838 P1, REPAIRED THE CROSSBEAM. MAJOR REPAIR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N655FE/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 = 'N655FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N655FE/reports

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