# Service difficulty reports: N276UP

A list on [N276UP](https://openairdocs.org/aircraft/N276UP.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 · 307 reports

- [SDR IPXA202507304352](https://openairdocs.org/sdr/IPXA202507304352.md): Transmitter · faulted · Jul 29, 2025 · N276UP · Doug MD11F · Trailing Flap Position Indicating System
  > DURING ILS COUPLED APPROACH WITH FLAPS AT 35 AND VERIFIED BY CAPT AND F/O GREEN BOX, TOO LOW FLAPS WARNING WENT OFF TWICE CAUSING GO AROUND. REPLACED RT OTBD FLAP POSITION TRANSMITTER IAW MM 27-54-02-400-801.
- [SDR IPXA2025030716718](https://openairdocs.org/sdr/IPXA2025030716718.md): Fan · faulted · Mar 7, 2025 · N276UP · Doug MD11F · Air Distribution Fan
  > DURING DESCENT, "AVNCS FAN OVRD" ALERT ILLUMINATED. -END- INSPECTED AVIONICS ACCESS DOOR, MAIN CARGO AND ALL 3 LOWER CARGO COMPARTMENT DOOR SEALS. FOUND SEVERAL SMALL AREAS WHERE SEAL WAS DISLODGED. RESECURED IAW MM 52-00-00. C/W FIM 21-26-00-1 FIG 106. NO FAU
- [SDR IPXA202412235686](https://openairdocs.org/sdr/IPXA202412235686.md): Indicator · inoperative · Dec 21, 2024 · N276UP · Doug MD11F · Emergency Equipment
  > L1 DOOR LIGHT TEST BUTTON FOR SLIDE INOP. R/R L1 DOOR SLIDE PRESSURE TEST INDICATOR AND PERFORMED THE OPS CK IAW AMM 25-61-04. OPS CK GOOD.
- [SDR IPXA2024091855880](https://openairdocs.org/sdr/IPXA2024091855880.md): Packing · inoperative · Sep 17, 2024 · N276UP · Doug MD11F · Escape Slide
  > L1 SLIDE REQUIRES REMOVAL DUE TO INOP PACKING AND CAUSING LINER TO BULGE REPLACED L1 DOOR EVACUATION SLIDE/RAFT ASSY AND CONTAINER IAW AMM 25-61-01. FUNCTIONAL CHECKS GOOD. THIS CLEARS MEL, PLACARD REMOVED. C/W RII REQUIREMENTS IAW GMM 04-02/25
- [SDR IPXA2024090630691](https://openairdocs.org/sdr/IPXA2024090630691.md): Filter · odor · Sep 5, 2024 · N276UP · Doug MD11F · Air Distribution System
  > DURING FLIGHT WE DETECTED AN ACRID ELECTRICAL SMELL FROM THE GALLEY AREA. WE TROUBLESHOT AND REMOVED POWER FROM THE GALLEY VIA THE CABIN BUS SWITCH. FUMES CONTINUED. DONNED 02 DIVERTED TO MHR. PERFORMED TECH ALERT T3F18E0054RL4 NO DISCREPANCIES FOUND REPLACED
- [SDR IPXA2024090530978](https://openairdocs.org/sdr/IPXA2024090530978.md): Slide · no discrepancy · Sep 5, 2024 · N276UP · Doug MD11F · Cabin Equipment/Furnishings
  > SLIDE MANUALLY DEPLOYED BY FLIGHT CREW AFTER EMERGENCY LANDING IN MHR REF T3F18E0054QNA. R&R'D L1 DOOR EVAC SLIDE PER AMM 25-61-01
- [SDR IPXA2024090530691](https://openairdocs.org/sdr/IPXA2024090530691.md): Unknown · odor · Sep 5, 2024 · N276UP · Doug MD11F · Air Distribution System
  > DURING FLIGHT WE DETECTED AN ACRID ELECTRICAL SMELL FROM THE GALLEY AREA. WE TROUBLESHOT AND REMOVED POWER FROM THE GALLEY VIA THE CABIN BUS SWITCH. FUMES CONTINUED. DONNED 02 DIVERTED TO MHR.
- [SDR IPXA2024062965695](https://openairdocs.org/sdr/IPXA2024062965695.md): Test Switch · faulted · Jun 28, 2024 · N276UP · Doug MD11F · Emergency Equipment
  > R1 DOOR EVACUATION SLIDE PRESS TO TEST SWITCH DOES NOT ILLUMINATE REPLACED BATTERIES ON R1 REMOTE PRESSURE INDICATOR ASSEMBLY IAW AMM 25-61-04. OP CHECK GOOD.
- [SDR IPXA2024060751273](https://openairdocs.org/sdr/IPXA2024060751273.md): Shutoff Valve · failed · Jun 7, 2024 · N276UP · Doug MD11F · Ice/Rain Protection System
  > *AIR TURN BACK* *IN FLIGHT SHUTDOWN* *EMERGENCY DECLARED* LOGBOOK ITEM - G38901 ITEM 1 - AFTER TAKEOFF RECEVED A LEVEL 1 ENG 2 A-ICE DURING CLIMB WHILE RUNNING THAT CHECK LIST. WE RECEVED A LEVEL 3 ENG 2 A-ICE DUCT. SHUT DOWN #2 ENG PER CHECK LIST. VERIFIED S
- [SDR IPXA2024061271724](https://openairdocs.org/sdr/IPXA2024061271724.md): Indicator · inoperative · Jun 3, 2024 · N276UP · Doug MD11F · Escape Slide
  > R1 DOOR EMERGENCY SLIDE INDICATING LIGHT IS INOP ATA25-61 REMOVED AND REPLACED R1 DOOR EMERGENCY SLIDE REMOTE PRESSURE INDICATOR SWITCH LIGHT ASSY, PERFORMED OPS CHECK OF R1 DOOR EMERGENCY SLIDE REMOTE PRESSURE INDICATOR SWITCH LIGHT ASSY, OPS CHECK GOOD IN RE
- [SDR IPXA2024060471724](https://openairdocs.org/sdr/IPXA2024060471724.md): Indication Sys · inoperative · Jun 3, 2024 · N276UP · Doug MD11F · Emergency Equipment
  > R1 DOOR EMERGENCY SLIDE INDICATING LIGHT IS INOP ATA25-61 VERIFIED STEP 3
- [SDR IPXA2024051044954](https://openairdocs.org/sdr/IPXA2024051044954.md): Bolt · sheared · Apr 30, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > RH O/B FLAP I/B HINGE FWD BOLT IS BROKEN ATA 57-55. VERIFIED REMOVED AND REPLACED R/H O/B FLAP I/B FWD HINGE BOLT P/N ARC0882-501 BATCH: 0004096187 IN REF TO UPS MD11 AMM 57-53-01-400-801 TW ID:19-411 CAL DUE: 16-AUG-2024.
- [SDR IPXA2024052211513](https://openairdocs.org/sdr/IPXA2024052211513.md): Support Fitting · corroded · Apr 27, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > FOUND CORROSION ON R/H SIDE SUPPORT FOR O/B FLAP I/B FWD FLAP HINGE ATA 57-55 REMOVE AND REPLACE SUPPORT P/N ARB0029-510 PER MD11 AMM 57-53-01-400-801 AND SRM 51-30 REQUIREMENTS.
- [SDR IPXA2024051808924](https://openairdocs.org/sdr/IPXA2024051808924.md): Attach Angle · broken · Apr 21, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > FLAP SIDE O/B FLAP I/B HINGE CAGE O/B "S" PANEL ATTACHED ANGLE BROKEN ATA 57-50 ACCOMPLISH EO-90304-REQ1 (VT-SAA EA 011-5753-01-B0201 I/R). ANGLE BRACKET INSTALLATION ON EA: 011-5753-01-B0201 REVISION P1 STEP 5.
- [SDR IPXA2024052395849](https://openairdocs.org/sdr/IPXA2024052395849.md): Hinge Bracket · corroded · Apr 20, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > FLAP EO - R/H O/B FLAP O/B FWD HINGE #4 LUG BORE HAS CORROSION (114-79) ATA 57 REMOVE AND REPLACE HINGE BRACKET ASSEMBLY P/N ARC0503-504 PER MD11 AMM 57-53-01 REV 96.
- [SDR IPXA2024052395650](https://openairdocs.org/sdr/IPXA2024052395650.md): Hinge Bracket · corroded · Apr 20, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > FLAP EO - R/H O/B FLAP I/B FWD HINGE #4 LUG BORE HAS CORROSION (114-75) ATA 57 REMOVE AND REPLACE HINGE BRACKET ASSEMBLY, ARC0502-508, PER MD11 AMM 57-53-01/401 REV 96.
- [SDR IPXA2024052389264](https://openairdocs.org/sdr/IPXA2024052389264.md): Hinge · corroded · Apr 19, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > FLAP EO - L/H O/B FLAP OB FWD HINGE O/B #8 LUG BORE IS WORN (114-53) ATA 57 REPAIR ACCOMPLISHED TO L/H WING O/B FLAP O/B FWD HINGE REF SREO-87943-REQ001 REF LINE#1451.
- [SDR IPXA2024052389256](https://openairdocs.org/sdr/IPXA2024052389256.md): Hinge · corroded · Apr 19, 2024 · N276UP · Doug MD11F · Trailing Edge Flaps
  > FLAP EO - L/H O/B FLAP O/B FWD HINGE I/B #8 LUG BORE HAS CORROSION (114-51) ATA 57 REPAIR ACCOMPLISHED TO L/H WING O/B FLAP O/B FWD HINGE REF SREO-87943-REQ001 REF LINE#1450.
- [SDR IPXA2024051051043](https://openairdocs.org/sdr/IPXA2024051051043.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X46/STR52. ACCOMPLISHED REPAIR PER EO-90346-REQ1 AND VT-SAA EA 011-5710-01-B0198, REV. I/R.
- [SDR IPXA2024060451189](https://openairdocs.org/sdr/IPXA2024060451189.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuel Storage
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X46/STR49. (015-79) ATA 57. INSTALLED 1EA STRINGER SECTION, 2EA "C" ANGLES REPAIR SPLICE, 2EA "Z" ANGLES REPAIR SPLICE AND 2 EA FITTINGS, AT UPPER CTR AUX TANK, STA X17 AND X46 STR 49 PER REF MD
- [SDR IPXA2024053150485](https://openairdocs.org/sdr/IPXA2024053150485.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuel Storage
  > [STR] UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-46 AND X-81/STR44. ACCOMPLISHED REPAIR PER MD-11 SRM 57-10-03-2R-1 REPAIR 1, FIGURE 201 (REVISION 70). AUDIT C/W
- [SDR IPXA2024053150690](https://openairdocs.org/sdr/IPXA2024053150690.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuel Storage
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-17 AND X-46/STR47. (015-74) ATA 57. INSTALLED ALL STR. 47 REPAIR PARTS AND REINSTALLED 2 EXISTING SHEAR TIES AT UPPR CENTER AUXILIARY TANK BETWEEN STA. X-30 TO X-57 IAW MD11 SRM 57-10-03-2R-1. ACCOMP
- [SDR IPXA2024052546477](https://openairdocs.org/sdr/IPXA2024052546477.md): Floor Support · corroded · Apr 17, 2024 · N276UP · Doug MD11F · Fuselage Miscellaneous Structure
  > COURIER FLOOR AREA FWD OF R1 DOOR UNDER LAVATORY HAS CORROSION. INSTALLED FLOOR SUPPORT AT CURIER AREA FWD OF RI DOOR UNDER LAVATORY IAW SRM 51-33-01-51-35-01. REMOVED AND REPLACED FLOOR SUPPOR IAW DWG ABA7341, DWG SP11530074 AND SRM 5100 GUIDELINES.
- [SDR IPXA2024052246418](https://openairdocs.org/sdr/IPXA2024052246418.md): Skin · corroded · Apr 17, 2024 · N276UP · Doug MD11F · Fuselage Main, Plate/Skin
  > MAIN CABIN CTR WING BOX AREA HAS CORROSION ON R/H SIDE BETWEEN STA 1199 - 1219 AND 106 INCH. ACCOMPLISHED REPAIR PER EO-90345-REQ1 AND VT-SAA EA 011-5730-01-B0194, REV I/R.
- [SDR IPXA2024051851130](https://openairdocs.org/sdr/IPXA2024051851130.md): Tank · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuel Storage
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X46/STR50. INSTALLED 1EA STRINGER SECTION, 2EA "Z" REPAIR ANGLE SPLICE, 2EA "C" ANGLE REPAIR SPLICE, AND 2EA FITTING, AT UPPER CTR AUX TANK BTW STA X17 AND X46 STR 50 PER REF MD-11 SRM 57-10-03
- [SDR IPXA2024051750844](https://openairdocs.org/sdr/IPXA2024051750844.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuel Storage
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X-17/STR47. (015-75) ATA 57. INSTALLED ALL STR. 47 REPAIR PARTS AND REINSTALLED 2 EXISTING SHEAR TIES AT UPPR CTR AUX TANK BETWEEN STA X3 TO X30 IAW MD11 SRM 57-10-03-2R-1.
- [SDR IPXA2024051850618](https://openairdocs.org/sdr/IPXA2024051850618.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-17 AND X-46/STR50. (015-73) ATA 57. INSTALLED 1 EA STRINGER SECTION, 2 EA "C" ANGLE REPAIR SPLICE, 2 EA "Z" ANGLE REPAIR SPLICE AND 2 EA FITTING, AT UPPER CENTER AUX TANK STA BTW X-17 AND X-46 PER REF
- [SDR IPXA2024051741145](https://openairdocs.org/sdr/IPXA2024051741145.md): Sprocket · worn · Apr 17, 2024 · N276UP · Doug MD11F · Passenger/Crew Doors
  > WORN OUT SPROKET FOR L1 DOOR AFT CLOSURE MECHANISM. REMOVED AND REPLACED 2 EA SPROCKETS ON L1 DOOR AFT CLOSURE MECHANISM DRIVE CHAIN PER. MD-11 DWG ABA7941 REV. S AND ADJUSTED PER. MD-11 AMM 52-11-02-830-801.
- [SDR IPXA2024051049553](https://openairdocs.org/sdr/IPXA2024051049553.md): Skin · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Wing, Plate/Skin
  > WHILE ACCOMPLISHING TASK CARD MXP-7682-JIC FOUND 5 EA CRACKED HOLES ON FUEL LANDING AS MARKED ON PART WITH TAPE. ATA 57-20. INSTALLED 5EA BUSHING REPAIR AT R/H WING FUEL ACCESS PANEL 636AB REF. MD-11 SRM 57-20-02-2R-5 REPAIR 5.
- [SDR IPXA2024051050552](https://openairdocs.org/sdr/IPXA2024051050552.md): Stringer · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-17 AND X-46/STR52. ACCOMPLISHED PER EO-90379-REQ1 AND VT-SAA EA 011-5710-01-B0193, REV. I/R.
- [SDR IPXA2024041849724](https://openairdocs.org/sdr/IPXA2024041849724.md): Landing · cracked · Apr 17, 2024 · N276UP · Doug MD11F · Wing Main, Frame Structure
  > WHILE ACCOMPLISHING TASK CARD MXP-7633-JIC FOUND 2 EA CRACKED HOLES ON FUEL LANDING AS MARKED ON PART WITH TAPE. ATA. 57-20. INSTALLED 2 EA BUSHING REPAIR AT L/H WING FUEL ACCESS PANEL 536AB REF. MD-11 SRM 57-20-02-2R-5 REPAIR 5.
- [SDR IPXA2024041741145](https://openairdocs.org/sdr/IPXA2024041741145.md): Sprocket · worn · Apr 17, 2024 · N276UP · Doug MD11F · Passenger/Crew Doors
  > APG - WORN OUT SPROCKET FOR L1 DOOR AFT CLOSURE MECHANISM ATA 52-10.
- [SDR IPXA2024060130995](https://openairdocs.org/sdr/IPXA2024060130995.md): Spar Cap · corroded · Apr 16, 2024 · N276UP · Doug MD11F · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER LOWER BARREL NUT, 2ND FROM REAR, HAS EXTENSIVE CORROSION IN ITS CAVITY. CAP/PLUG IS BLOWN OUT. ACCOMPLISHED REPAIR PER EO-90520-REQ1 (EA 011-5510-01-B0186, REV. IR).
- [SDR IPXA2024060130410](https://openairdocs.org/sdr/IPXA2024060130410.md): Spar Cap · corroded · Apr 16, 2024 · N276UP · Doug MD11F · Horizontal Stabilizer, Spar/Rib
  > CAP/ PLUG IS COMING OUT OF ITS BORO PLUG HOLE, FRONTMOST, UNDERSIDE OF HORIZONTAL STAB/ TAIL TANK, RT SIDE. ACCOMPLISHED REPAIR PER EO-90209-REQ1 AND EA 011-5510-01-B0189, REV. IR.
- [SDR IPXA2024060130520](https://openairdocs.org/sdr/IPXA2024060130520.md): Spar Cap · corroded · Apr 16, 2024 · N276UP · Doug MD11F · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER LOWER BARREL NUT, R/H REARMOST POSITION, HAS EXTENSIVE CORROSION IN ITS CAVITY. CAP/ PLUG IS BLOWN OUT. ACCOMPLISHED REPAIR PER EO-90521-REQ1 (EA 011-5510-01-B0188, REV. IR).
- [SDR IPXA2024060130121](https://openairdocs.org/sdr/IPXA2024060130121.md): Spar Cap · corroded · Apr 16, 2024 · N276UP · Doug MD11F · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER LOWER BARREL NUT, 2ND FROM REAR, HAS EXTENSIVE CORROSION IN ITS CAVITY. CAP/ COVER IS BLOWN OUT. REPAIR ACCOMPLISHED PER EO-90521-REQ1 (EA 011-5510-01-B0188, REV. IR).
- [SDR IPXA2024060131048](https://openairdocs.org/sdr/IPXA2024060131048.md): Spar Cap · corroded · Apr 16, 2024 · N276UP · Doug MD11F · Horizontal Stabilizer, Spar/Rib
  > CAP/ PLUGS ARE COMING OUT OF THEIR BORO PLUG HOLES, 1ST AND 2ND FROM FRONT, UNDERSIDE OF HORIZONTAL STAB/ TAIL TANK, LT SIDE. MKD AS DB-1Z AND DB-1E. ACCOMPLISHED REPAIR PER EO-90205-REQ1 AND VT-SAA EA 011-5510-01-B0187, REV. IR.
- [SDR IPXA2024060130260](https://openairdocs.org/sdr/IPXA2024060130260.md): Panel · corroded · Apr 16, 2024 · N276UP · Doug MD11F · Elevator Structure
  > CAP/ PLUG IS COMING OUT OF ITS BORO PLUG HOLE, 3RD FROM BACK, UNDERSIDE OF HORIZONTAL STAB/ TAIL TANK, RT SIDE. ACCOMPLISHED REPAIR PER EO-90203-REQ1 AND VT-SAA EA 011-5510-01-B0190, REV. IR.
- [SDR IPXA2024052567973](https://openairdocs.org/sdr/IPXA2024052567973.md): Cap · corroded · Apr 12, 2024 · N276UP · Doug MD11F · Wing Miscellaneous Structure
  > LEFT WING XORS 345-433 LWR T.E. AREA TEE CHANNEL HAS MULTIPLE CORROSION AND SINGLE CRACKED. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE AT GUSSET IAW SRM 57-50-02-2R-9. INSTALLED 1 EA TEE CHANNEL, SIX PANEL ACCESS, THREE ANGLES, THREE STIFFENERS, THREE REPAI
- [SDR IPXA2024050268880](https://openairdocs.org/sdr/IPXA2024050268880.md): Frame · cracked · Apr 12, 2024 · N276UP · Doug MD11F · Fuselage Main, Frame
  > FWD AVIONIC COMP INSIDE AREA STA 457-475 RH SIDE FUSELAGE FRAME HAS CRACKED. 74-026 ATA CODE 53. ACCOMPLISHED REPAIR REF. EO-90200-REQ1 (VT-SAA EA 011-5310-01-B0191, REV. IR).
- [SDR IPXA2024050377941](https://openairdocs.org/sdr/IPXA2024050377941.md): Support Channel · damaged · Apr 12, 2024 · N276UP · Doug MD11F · Cargo Compartments
  > TWO HOLES BLOWN OUT OF LOWER FWD CARGO BAY CEILING PANEL SUPPORT CHANNEL, BS 989 IN POSITION 4 AREA. ACCOMPLISH REPAIR PER EA 011-5300-01-B0192, REV I/R, AND EO-90199-REQ1, REV 1.
- [SDR IPXA2024011646225](https://openairdocs.org/sdr/IPXA2024011646225.md): Unknown · unknown · Jan 16, 2024 · N276UP · Doug MD11F · Emergency Equipment
  > L1 DOOR ASSIST BOTTLE PRESSURE LOW SERVICED L1 DOOR BOTTLE AS REQ€™D REF AMM 12-25-04
- [SDR IPXA2023112874850](https://openairdocs.org/sdr/IPXA2023112874850.md): Unknown · unknown · Nov 28, 2023 · N276UP · Doug MD11F · Escape Slide
  > D1L EVACUATION SLIDE PRESSURE PRESS TO TEST SWITCH U/S. C/W DMP IAW MEL 25-61-2. PRESSURE CHECKS GOOD.
- [SDR IPXA2023110774176](https://openairdocs.org/sdr/IPXA2023110774176.md): Unknown · unknown · Nov 7, 2023 · N276UP · Doug MD11F · Escape Slide
  > DOOR R1 SLIDE/RAFT INDICATOR LIGHT DID NOT ILLUMINATE DURING PRE-FLIGHT TEST. REMOVED AND INSTALLED R1 SLIDE/RAFT INDICATOR LIGHT ASSY. OPS CHECK GOOD. NO DEFECTS NOTED. PER AMM 25-61-04/401
- [SDR IPXA2023022291240](https://openairdocs.org/sdr/IPXA2023022291240.md): Girt Bar · inoperative · Feb 21, 2023 · N276UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:NAL1 DOOR GIRT BAR DISCONNECTED ON RIGHT SIDE.T/S DISCREPANCY & DETERMINED IT WAS THE MANUAL LIFT BAR THAT WAS OUT OF POSITION. REINSTALLED MANUAL LIFT BAR AS REQ'D I/A/W AMM 25-61-01-400-801.
- [SDR IPXA2023020290534](https://openairdocs.org/sdr/IPXA2023020290534.md): Light · inoperative · Feb 2, 2023 · N276UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NA*SUPPLEMENTAL SDR* *DOES NOT INITIATE TEST WHEN PUSHED* REF M-801780 EMGY LIGHTING SYS TEST EACH FLT REINSPECT REQUIRED. C/W EACH FLT REINSPECTION OF EMGCY LIGHT SYS TEST PER DMP 33-50-2. DEFERRAL REMAINSR/R EMERGENCY LIGHT TEST PUSHBUTTON SW
- [SDR IPXA2023020390576](https://openairdocs.org/sdr/IPXA2023020390576.md): Switch · inoperative · Feb 2, 2023 · N276UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NA** SUPPLEMENTAL SDR ** EMER LT TEST SWITCH DOES NOT INITIATE TEST WHEN PUSHED. WORKS INTERMITTENTLY. EMERGENCY LIGHTS TEST FUNCTION DEFERRED IAW MEL 33-50-2. DMP ACCOMPLISHED CONTROL #M801780 ASSIGNED. PLACARD INSTALLED.R/R EMERGENCY LIGHT TE
- [SDR IPXA2023011890016](https://openairdocs.org/sdr/IPXA2023011890016.md): Floor Panel · damaged · Jan 16, 2023 · N276UP · Doug MD11F · Fuselage Floor Panel
  > FLOOR PANEL IS REMOVED AT MCD POSITON 12R, PART NUMBER AFA 7413-34FABRICATION OF FLOOR PANEL TRANSFERRED OVER TO SHEETMETAL SHOP N/R 684246 P/N AFA 74BYY THIS IS A MAJOR REPAIR. 4238767, 1-14-23] FILE 4 ACCOMPLISHED FLOOR PANEL FABRICATION PER EO MD11-5320-27
- [SDR IPXA2023011890015](https://openairdocs.org/sdr/IPXA2023011890015.md): Floor Panel · damaged · Jan 16, 2023 · N276UP · Doug MD11F · Fuselage Floor Panel
  > FLOOR PANEL DAMAGED MAIN DECK CARGO POSITON 12R -FABRICATION FLOOR PANEL REF # AEA 0177-173 TRANSFER TO N/R ON SHEETMETAL SHOP # 684245 THIS IS A MAJOR REPAIR. 4235767 1-14-23] FILEY ACCOMPLISHED FLOOR PANEL FABRICATION PER EO MD11-5320-27386-C ON NRC 684245.
- [SDR IPXA2023011689949](https://openairdocs.org/sdr/IPXA2023011689949.md): Seat Track · broken · Jan 16, 2023 · N276UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, SEAT TRACK BROKEN MAIN CARGO DECK CARGO POS 12R. REPAIRED IAW EO MD11-5310-85688-A.

Next page: https://openairdocs.org/aircraft/N276UP/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 = 'N276UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N276UP/reports

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