# Service difficulty reports: N275UP

A list on [N275UP](https://openairdocs.org/aircraft/N275UP.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 7 · 322 reports

- [SDR IPXA2025110768137](https://openairdocs.org/sdr/IPXA2025110768137.md): Pulley · damaged · Nov 7, 2025 · N275UP · Doug MD11F · Passenger/Crew Doors
  > LEFT ENTRY DOOR MAKES GRINDING NOISE WHILE OPENING REMOVED BOTH FWD DRIVE CABLES FROM CABLE DRUM. REMOVED AND REPLACED DAMAGED FWD LWR DRIVE CABLE PER AMM 52-11-03. REMOVED AND REPLACED DAMAGED PULLEYS IN REFERENCE TO AMM 52-11-03. REINSTALLED UPPER FWD DRIV
- [SDR IPXA2025100222743](https://openairdocs.org/sdr/IPXA2025100222743.md): Seat Track · corroded · Sep 15, 2025 · N275UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CENTER CARGO COMPARTMENT. SEAT TRACK LOCATED ON CEILING AREA BETWEEN STA 1541 AND 1561/LBL8 HAS CORROSION. HFEC SURFACE INSPECTED SEAT TRACK CUT OUT PER NDTSPM 06-10-01.001.FABRICATED SEAT TRACK SPLICE AND SPLICE PLATE REF MD11 SRM 53-00-52-2R-1.INSTALLED EWI
- [SDR IPXA2025100322180](https://openairdocs.org/sdr/IPXA2025100322180.md): Seat Track · corroded · Sep 15, 2025 · N275UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LOCATED AT STA 2007/LBL70 HAS CORROSION. VERIFIED STEP 31 C/W PER UPS GMM RII 04-02
- [SDR IPXA2025100322188](https://openairdocs.org/sdr/IPXA2025100322188.md): Seat Track · corroded · Sep 15, 2025 · N275UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, WASTE TANK COMPARTMENT. SEAT TRACK LOCATED AT BS 2007, RBL70 HAS CORROSION. ACCOMPLISHED REPAIR PER EO-95277-REQ1 REV 2 (T3F18E007K49S) AND VT-SAA EA 011-5342-01-B0567, REV A.
- [SDR IPXA2025100256077](https://openairdocs.org/sdr/IPXA2025100256077.md): Doubler · cracked · Sep 11, 2025 · N275UP · Doug MD11F · Wing, Plate/Skin
  > L/H WING. FIXED L/E INNER SKIN BEADED DOUBLER LOCATED APPROX STA XORS 402 HAS CRACK. VERIFIED STEP 25 VERIFIED REPAIR WAS ACCOMPLISH REPAIR PER MD-11 SRM 57-40-02-2R FIGURE 205 REPAIR 15 REV 72.
- [SDR IPXA2025100255936](https://openairdocs.org/sdr/IPXA2025100255936.md): Doubler · cracked · Sep 11, 2025 · N275UP · Doug MD11F · Wing, Plate/Skin
  > L/H WING. FIXED L/E INNER SKIN BEADED DOUBLER LOCATED APPROX STA XORS 506 HAS CRACK. OUT OF SEQUENCE STEP 3 C/W IAW UPS RII GMM 04-02. ACCOMPLISHED REPAIR PER MD-11 SRM 57-40-02-2R FIGURE 205 REPAIR 15 REV 71
- [SDR IPXA2025071911037](https://openairdocs.org/sdr/IPXA2025071911037.md): Door · handler error · Jul 19, 2025 · N275UP · Doug MD11F · Passenger/Crew Doors
  > L-1 DOOR WAS ACTIVATED TO THE EMERGENCY POSITION BY GROUND LOAD CREW SERVICED DOOR ASSIST BOTTLE FOR L-1 DOOR IAW AMM 12-25-04-600-801. OK FOR SERVICE PLACARD REMOVED THIS CLOSES T3F18E0072JY8
- [SDR IPXA2025032534685](https://openairdocs.org/sdr/IPXA2025032534685.md): Battery · discharged · Mar 25, 2025 · N275UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO PREFLIGHT. REVERSED DMP AND R&R EMERGENCY LT BATTERY PER AMM 33-51-01. OPS CHECK GOOD.
- [SDR IPXA2024051842150](https://openairdocs.org/sdr/IPXA2024051842150.md): Battery · no test · May 18, 2024 · N275UP · Doug MD11F · Emergency Lighting
  > DURING PDC, FOUND "EMER LT BAT 1 LO" WHEN TESTING EMERGENCY LIGHTING SYSTEM. REVERSED DMP. R/R EMERGENCY POWER SUPPLY BATTERY REF MM 33-51-01. OPS CK OK. DEFERRAL CLEARED, PLACARD REMOVED.
- [SDR IPXA2024012647104](https://openairdocs.org/sdr/IPXA2024012647104.md): Actuator · unserviceable · Jan 26, 2024 · N275UP · Doug MD11F · Leading Edge Slat Actuator
  > AIR TURN BACK.AFTER TAKEOFF WHEN FLAPS AND SLATS RETRACTED, LEVEL 2 €ŒAIL DEFLECT DISAGREE€? ALERT DISPLAYED.RAN QRH PROCEDURE TO RESET, NO HELP.AIRCRAFT HAD ROLL TO THE RIGHT THROUGHOUT THE RETURN FLIG VERIFIED INSTALL AND SAFETIES, WITNESSED RIG, OPS CHECK
- [SDR IPXA2023110758601](https://openairdocs.org/sdr/IPXA2023110758601.md): Spar Cap · corroded · Oct 12, 2023 · N275UP · Doug MD11F · Wing Spar
  > *MAJOR REPAIR* RH UPPER WING REAR SPAR HAS CORROSION 13" FWD OF O/B AILERON O/B SIDE. 49-044 (STR). ACCOMPLISHED EO-88539-REQ1, AND EA#011-5710-01-B0114, REV. IR, AUDIT COMPLETE
- [SDR IPXA2023110429669](https://openairdocs.org/sdr/IPXA2023110429669.md): Unknown · unknown · Oct 11, 2023 · N275UP · Doug MD11F · Flight Control System
  > RH LE COVE HAS A CRACKED BEADED DOUBLER AT FASTENER AT APPROX XOS 670. 49-033 ACCOMPLISH REPAIR TO THE RH WING FIXED LE BEADED DOUBLER BETWEEN XOS=667.6 TO XOS=673.7 PER MD11 SRM 57-40-02, REPAIR 15, REV 70. INSTALLED REPLACEMENT BEADED DOUBLER AT R/H WING L
- [SDR IPXA2023110429401](https://openairdocs.org/sdr/IPXA2023110429401.md): Doubler · cracked · Oct 11, 2023 · N275UP · Doug MD11F · Wing Structure
  > *SDR FILED OPEN* RH LE COVE HAS A CRACKED BEADED DOUBLER AT FASTENER AT APPROX XOS 613. 49-032 C/W STEP 15
- [SDR IPXA2023110431678](https://openairdocs.org/sdr/IPXA2023110431678.md): Doubler · cracked · Oct 11, 2023 · N275UP · Doug MD11F · Wing Structure
  > RH LE COVE HAS A CRACKED BEADED DOUBLER AT FASTENER AT APPROX XOS 690. 49-034 ACCOMPLISH REPAIR OF THE RH WING FIXED LE BEADED DOUBLER BETWEEN XOS=692.038 TO XOS=698.127 PER MD11 SRM 57-40-02, REPAIR 15, REV 70 AND BOEING SR ID 3-4484182131. REVIEWED
- [SDR IPXA2023100350779](https://openairdocs.org/sdr/IPXA2023100350779.md): Not Reported · not reported · Oct 2, 2023 · N275UP · Doug MD11F · Emergency Lighting
  > L1 DOOR MOVABLE CEILING EMERGENCY EXIT SIGN BROKEN OFF. REMOVED AND REPLACED L1 DOOR EXIT SIGN IAW AMM 33-27-05. OPS CHECK GOOD.
- [SDR IPXA2023092694249](https://openairdocs.org/sdr/IPXA2023092694249.md): Battery · discharged · Sep 25, 2023 · N275UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 10. PLACED EMERGENCY LIGHTING SYSTEM ON DEFERRAL IAW MEL 33-50-4 C/B'S PULLED J1 CONNECTOR REMOVED & STOWED CONTROL #M812697 ASSIGNEDR&R EMERGENCY BATTERY SUPPLY POWER PER AMM 32-51-01 OPS CK GOOD PLACARD REMOVED DMP REVERSED THIS CLEARS M 812697
- [SDR IPXA2023020390562](https://openairdocs.org/sdr/IPXA2023020390562.md): Fire Warning · warning light · Jan 27, 2023 · N275UP · Doug MD11F · Air Conditioning System
  > INSPECTION TYPE:NA*ATB* *A/C WAS OOS* CAPT / CREW EXPERIANCE SUSPECT SMOKE IN COCKPIT SHORYLY AFTER DEPARTURE DECLARED EMERGENCY AFTER LEVEL 3 LOWER AFT CARGO FIRE WARNING RESULTED & ATB " UPON LANDING EMERGECNY EGRESS VIA SLIDE PULLED ALL ENGINES & APU FIRE H
- [SDR IPXA2023013090362](https://openairdocs.org/sdr/IPXA2023013090362.md): Slide · unwanted deploy · Jan 27, 2023 · N275UP · Doug MD11F · Escape Slide
  > L1 DOOR SLIDE DEPLOYED. R&R L1 DOOR SLIDE IAW AMM 25-61-01. OK FOR SERVICE. EFF SOURCE REF: 25-61-05-01.
- [SDR IPXA2022120288633](https://openairdocs.org/sdr/IPXA2022120288633.md): Door · unsecure · Dec 1, 2022 · N275UP · Doug MD11F · Landing Gear Doors
  > ATB AT 18,000, THERE WAS A TREMENDOUS THUMP THEN EXTREME VIBRATIONS THRU OUT THE AIRPLANE FOUND NLG DOOR DAMAGED. REMOVED L FWD NLG DOOR IAW AMM 32-23-03. REPLACED LT NLG FWD DOOR AND ATTACHMENTS IAW AMM 32-23-03. CK OK FOR SVC. ORIG SUB DATE: 12/2/2022
- [SDR IPXA2022102587498](https://openairdocs.org/sdr/IPXA2022102587498.md): Switch · no test · Oct 24, 2022 · N275UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:N/ASLIDE TEST SWITCH ON R1 DOOR DOES NOT ILLUMINATE WHEN PUSHED TO TEST SLIDEEVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST IND SYS. INOP PLACED ON MEL 25-61-2. PLACARD INSTALLED DMP 25-61-2B PERFORMED, ACCOMPLISHED
- [SDR IPXA2022090986067](https://openairdocs.org/sdr/IPXA2022090986067.md): None · inoperative · Sep 9, 2022 · N275UP · Doug MD11F · Detection System
  > INSPECTION TYPE:N/A**EMERGENCY DECLARED** REQUEST TO REPLACE FIRE DETECTION CONTROL UNIT #2 DUE TO #2 ENG. FIRE INDICATIONREPLACED # 2 FDCU PER AMM 26-11-02 UP STEP D.(2) ( DANIEL VRANA 0559143 9-8-22. COMPLETED INSTALLATION STEPS & OPS CHECK OK REF. MM 26-11-
- [SDR IPXA2022071984331](https://openairdocs.org/sdr/IPXA2022071984331.md): Brake Assy · abnormal · Jul 17, 2022 · N275UP · Doug MD11F · Landing Gear System
  > INSPECTION TYPE:NA**EMERGENCY DEC'D*AIRPORT CRASH, FIRE & RESCUE ON ARRIVAL*LANDING UNEVENTFUL**BRAKE DIFF TEMP LEVEL 1 ON INITIAL CLIMB FROM BDL BRAKES IN INTIAL CLIMB BRAKE #8 SIGNIFICANTLY WARMERCHANGED #8 BRAKE PER FIM 32 40 25. AMM 32 43 20 400 801 ESR IP
- [SDR IPXA2022061583147](https://openairdocs.org/sdr/IPXA2022061583147.md): Slide · inoperative · Jun 15, 2022 · N275UP · Doug MD11F · Escape Slide
  > DURING PDC FOUND R 1 DOOR SLIDE REMOTE PRESS. IND INOP. RELAMP NO HELP. R1 SLIDE PTT IND DEFERRED PER MEL 25-61-2. DMP 25-61-2 STEP 1A C/W. PLACARD INSTALLEDREPLACED BATTERY ON PUSH TO TEST. OPS GOOD IAW AMM 25-61-00.
- [SDR IPXA2021121476935](https://openairdocs.org/sdr/IPXA2021121476935.md): None · none · Dec 13, 2021 · N275UP · Doug MD11F · Air Distribution System
  > INSPECTION TYPE:N/A** SUPPLEMENTAL SDR **CRG FLO AFT DISAG. ITEM PLACED ON MEL 21-21-2. CONTROL # M766105 ASSIGNED, PLACARD INSTALLED.REPLACED MSC PER AMM 31-42-01, CHECKS GOOD. NO CRG FLO AFT DIASG ALERT SHONE DURING TESTING PER AMM 21-27-01 AND 21-27-02. PLA
- [SDR IPXA2021110975802](https://openairdocs.org/sdr/IPXA2021110975802.md): None · none · Nov 9, 2021 · N275UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:N/A** SUPPLEMENTAL SDR**FLGHT CREW REPORTED R1 EVACUATOIN SLIDE REMOTE PRESSURE PRESS TO TEST INDICATOR DOES NOT ILLUMINATE.DEFERRED R1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYSTEM PER MEL 25-61-2. C/W DMP 25-61-2REPLACED BA
- [SDR IPXA2021103075466](https://openairdocs.org/sdr/IPXA2021103075466.md): Stiffener · cracked · Oct 19, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:4CAFT CARGO VERTICAL STIFFENER AT STA 1841 & X= 25.0 IS CRACKED.REMOVED AND REPLACED CRACKED AFT CARGO VERTICAL STIFFENER AT STA 1841 & X= 25.0 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021102575321](https://openairdocs.org/sdr/IPXA2021102575321.md): Frame · corroded · Oct 19, 2021 · N275UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:4CAFT AVI COMPARTMENT FRAME CORRODED AT STA. 469.173 CANTED BETWEEEN LBL 10" AND RBL 10".REPAIRED CORRODED FRAME AT STA. 469.173 IAW MD-11 SRM 53-00-07 REPAIR 2,FIG 201,REV 68. (MAJOR).
- [SDR IPXA2021102875404](https://openairdocs.org/sdr/IPXA2021102875404.md): Skin · corroded · Oct 18, 2021 · N275UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:4CRT WING UPPER FORWARD SKIN HAS CORROSION BETWEEN STA.XORS 212 AND XORS 216 STRINGER 16.REPAIRED CORRODED RT WING UPPER SKIN IAW SRM 57-00-01 FIG. 1 AND 51-30-00 (MINOR).
- [SDR IPXA2021103075465](https://openairdocs.org/sdr/IPXA2021103075465.md): Doubler · cracked · Oct 16, 2021 · N275UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:4CRT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED O/B OF #12 SLAT TRACK.REMOVED AND REPLACED CRACKED RT WING FIXED L/E SKIN SPLICE DOUBLER O/B OF #12 SLAT TRACK IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021102975443](https://openairdocs.org/sdr/IPXA2021102975443.md): Doubler · cracked · Oct 16, 2021 · N275UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:4CRT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED O/B OF SLAT TRACK #10.REMOVED AND REPLACED CRACKED RT WING FIXED L/E SKIN SPLICE DOUBLER O/B OF SLAT TRACK #10 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021102875409](https://openairdocs.org/sdr/IPXA2021102875409.md): None · cracked · Oct 16, 2021 · N275UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 763.68 TO XOS. 768.27.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 763.68 TO XOS. 768.27 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2021102775376](https://openairdocs.org/sdr/IPXA2021102775376.md): None · cracked · Oct 13, 2021 · N275UP · Doug MD11F · Standard Practices/Structures
  > INSPECTION TYPE:2CL/H MLG W/W INTERCOSTAL BELOW UPPER FWD. BRAKE ACCUMULATOR IS CRACKED.REPAIRED INTERCOSTAL IAW SRM53-40-12 REPAIR 3 FIG. 201. (MINOR)
- [SDR IPXA2021102675336](https://openairdocs.org/sdr/IPXA2021102675336.md): Skin · none · Oct 13, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:2CEXTERIOR FUSELAGE SKIN INCOMING REPAIR REQUIRES PERMANENT REPAIR.REPAIRED INCOMING FUSELAGE SKIN REPAIR BETWEEN STA. 970 TO 9801 AND BETWEEN L-43R TO L-48R IAW VT-SAA EA 011-5310-01-A9409 REV. I/R AND UPS EO MD11-5310-80738-A. (MAJOR) REF FAA
- [SDR IPXA2021102675333](https://openairdocs.org/sdr/IPXA2021102675333.md): Stiffener · none · Oct 13, 2021 · N275UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:4CRT MLG W/W VERTICAL STIFFENER CRACK AT AFT BULKHEAD.REMOVED,FABRICATED AND REPACED CRACKED STIFFENER IAW MD-11 SRM 51-35-01 AND SRM 51-31-01 (MINOR).
- [SDR IPXA2021102575298](https://openairdocs.org/sdr/IPXA2021102575298.md): Stiffener · none · Oct 13, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:4CLT MLG W/W VERTICAL STIFFENER CRACK AT AFT O/B WALL.REMOVED,FABRICATED AND REPLACED CRACKED VERTICAL STIFFENER IAW MD-11 SRM 51-35-01 AND SRM 51-33-01 (MINOR).
- [SDR IPXA2021102175176](https://openairdocs.org/sdr/IPXA2021102175176.md): Floor Panel · none · Oct 13, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:4CMAIN CARGO AT RCB FLOOR PANEL HAS CORROSION BEWTEEN STA 475.000 TO STA 500.175 AND X=-17 TO X=-27.500.REPAIRED CORRORED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9404 REV I/R AND UPS EO MD11-533-81917-A (MINOR)
- [SDR IPXA2021072672098](https://openairdocs.org/sdr/IPXA2021072672098.md): Battery · discharged · Jul 25, 2021 · N275UP · Doug MD11F · Emergency Lighting
  > EMER LT BATT 1 LO, ILLUMINATED ON EMER LT TEST. TRANSFERED TO DEFERRAL 33-50-4 PER MEL, DMP COMPLIED WITH, PLACARD INSTALLED. CONTROLL NUMBER M751397R/R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS TEST GOOD. PLACARD REMOVED. M751397 CLOSE
- [SDR IPXA2021071871800](https://openairdocs.org/sdr/IPXA2021071871800.md): Skin · punctured · Jul 18, 2021 · N275UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SPSTA. 6-30 TO 6-50 BETWEEN LONG. 46R-47R SKIN IS BENT INWARDSACCOMPLISHED SPLICE REPAIR TO THE OUTER SKIN P/N ADA3139-503 PER EO MD11-5330-80805-A
- [SDR IPXA2021071771781](https://openairdocs.org/sdr/IPXA2021071771781.md): Fitting · corroded · Jul 6, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:SVFWD CARGO SIDE GUIDE RAIL SUPPORT FITTING AT STA 1009 AND BETWEEN LONGERON 41R & 42R IS CORRODED.REMOVED CORRODED FWD CARGO SIDE RAIL SUPPORT FITTING, FABRICATED AND INSTALLED REPLACEMENT FITTING AT STA 1099 BETWEEN LONGERON 41R & 42R IAW SRM
- [SDR IPXA2021071971847](https://openairdocs.org/sdr/IPXA2021071971847.md): Skin · damaged · Jul 2, 2021 · N275UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SVFORWARD LWR FUSELAGE SKIN DAMAGE BETWEEN STA.975-1129 BETWEEN LONG 40R-48R.REPAIRED DAMAGED FUSELAGE SKIN BETWEEN STA.975-1129 AND BETWEEN LONG 40R-48R IAW UPS EO MD11-5310-80738-A APPENDIX A AND 8100-9 (MAJOR).
- [SDR IPXA2021071571715](https://openairdocs.org/sdr/IPXA2021071571715.md): Tear Strap · torn · Jun 29, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SVFWD CARGO STA 6-50 TEAR STRAP AT LONGERON 44R IS TORN.REPAIRED TORN FWD CARGO STA 6-50 TEAR STRAP AT LONGERON 44R IAW SRM 51-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021071571714](https://openairdocs.org/sdr/IPXA2021071571714.md): Tear Strap · torn · Jun 29, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SVFWD CARGO STA 6-10 TEAR STRAP AT LONGERON 44R IS TORN.REPAIRED TORN FWD CARGO DSTA 6-10 TEAR STRAP AT LONGERON 44R IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021071871807](https://openairdocs.org/sdr/IPXA2021071871807.md): Splice · cracked · Jun 28, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:SVR/H SIDE FUSELAGE SKIN SPLICE DOUBLER AND PLATE IS CRACKED AND BENT AT STA 1129. BETWEEN L42R AND L48R.REPAIRED R/H SIDE FUSELAGE SKIN SPLICE DOUBLER AND PLATE AT STA 1129. BETWEEN L42R AND L48R IAW UPS EO # MD11-5310-80845-A.
- [SDR IPXA2021071571712](https://openairdocs.org/sdr/IPXA2021071571712.md): Tear Strap · bent · Jun 28, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SVFWD CARGO STA 1059 TEAR STRAP AT LONGERON 43R IS BENT.REPAIRED BENT FWD CARGO STA 1059 TEAR STRAP AT LONGERON 43R IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021071571711](https://openairdocs.org/sdr/IPXA2021071571711.md): Tear Strap · bent · Jun 28, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SVFWD CARGO STA 1039 TEAR STRAP AT LONGERON 42R IS BENT.REPAIRED BENT FWD CARGO STA 1039 TEAR STRAP AT LONGERON 42R IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021071571709](https://openairdocs.org/sdr/IPXA2021071571709.md): Tear Strap · torn · Jun 28, 2021 · N275UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SVFWD CARGO STA 1079 TEAR STRAP BETWEEN LONGERON 43R & 44R IS TORN.REPAIRED TORN FWD CARGO STA 1079 TEAR STRAP BETWEEN LONGERON 43R & 44R IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021071771780](https://openairdocs.org/sdr/IPXA2021071771780.md): Longeron · bent · Jun 18, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:SVFWD CARGO LONGERON 44R BETWEEN STA 1099 - 6-30 HAS DEFLECTION.REPAIRED DEFLECTED FWD CARGO LONGERON 44R BETWEEN STA 1099 - 6-30 IAW UPS EO MD11-5320-80859-A. REF. FAA FORM 8100-9 (MAJOR).
- [SDR IPXA2021071871808](https://openairdocs.org/sdr/IPXA2021071871808.md): Splice Plate · bent · Jun 18, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:SVR/H SIDE FUSELAGE SPLICE PLATE IS BENT AT STA 1129 JUST BELOW L44R.REPAIRED R/H SIDE FUSELAGE SPLICE PLATE AT STA 1129 JUST BELOW L44R IAW UPS EO #MD11-5310-80845-A.
- [SDR IPXA2021071971845](https://openairdocs.org/sdr/IPXA2021071971845.md): Skin · torn · Jun 18, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:SVFORWARD LWR FUSELAGE SKIN IS TORN AT STA.1002-6-50.00 LONG 41R-47R.REPAIRED TORN SKIN AT LOWER FUSELAGE STA.1002-6.50.00 LONG 41R-47R IAW UPS EO MD11-5310-80738-A AND 8100-9 (MAJOR).
- [SDR IPXA2021071971841](https://openairdocs.org/sdr/IPXA2021071971841.md): Finger Doubler · dented · Jun 18, 2021 · N275UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:SVFORWARD CARGO COMPARTMENT FINGER DOUBLER DENTED BETWEEN STA. 919-1019 BETWEEN LON41R-44R.REPAIRED DENTED FINGER DOUBLER BETWEEN STA.919-1019 LON 41R-44R IAW UPS EO MD11-5310-80738-A AND 8100-9 (MAJOR).

Next page: https://openairdocs.org/aircraft/N275UP/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 = 'N275UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N275UP/reports

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