# Service difficulty reports: N174UP

A list on [N174UP](https://openairdocs.org/aircraft/N174UP.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 · 182 reports

- [SDR IPXA2026091796946](https://openairdocs.org/sdr/IPXA2026091796946.md): Girt Bar · lack of lube · Sep 17, 2026 · N174UP · Airbus A300F4622R · Emergency Equipment
  > ENTRY DOOR WOULD NOT DISARM. PERFORMED OPERATIONAL TEST IAW AMM 52-73-00/0501, OPS TESTS GOOD BUT OPERATION WASN€™T COMPLETELY SMOOTH WHILE DISARMING EMERGENCY SLIDE. LUBRICATED GIRT BAR ON L1 DOOR IAW AMM 52-10-30/401. OPS TESTS GOOD. THIS CLOSES MEL, DMP R
- [SDR IPXA2026041476930](https://openairdocs.org/sdr/IPXA2026041476930.md): Fire Loop · faulted · Apr 7, 2026 · N174UP · Airbus A300F4622R · Fire Detection
  > AIR TURN BACK, ENG 2 LOOP B FAULT AFTER DEPARTURE. TRANSIENT INDICATION REF. ASM 26-12-00. AT 26WD, NR 2 ENGINE B NACELLE DETECTOR, FOUND 17VDC FROM TERMINAL A-C. FOUND CERAMIC INSULATOR CONTAMINATED. REPLACED 26WD IAW MM 26-12-12/401. RECHECKED VOLTAGE AT 26W
- [SDR IPXA2026010909964](https://openairdocs.org/sdr/IPXA2026010909964.md): Light · inoperative · Jan 8, 2026 · N174UP · Airbus A300F4622R · Emergency Lighting
  > LAV EMERGENCY LIGHT INOP REMOVED AND REPLACED LAV LIGHT ASSY OPS GO OK FOR SERVICE REF COMMS 33-24-05
- [SDR IPXA2025111453333](https://openairdocs.org/sdr/IPXA2025111453333.md): Light · no test · Nov 13, 2025 · N174UP · Airbus A300F4622R · Emergency Lighting
  > CABIN, SUPERNUMERARY EMERGENCY LIGHT WILL NOT TEST REF PS-1 STEP 24. EMERGENCY LIGHTS OPS CK. OK REVERSED DMP. T/S PER TSM 33-51-00 FIG 106, FOUND CONNECTOR ON P/B SW (25WL) INSTALLED UPSIDE DOWN. INSTALLED SWITCH REF ASM 33-51-00, OPS CK OK. DEFERRAL CLEARED
- [SDR IPXA2025100717233](https://openairdocs.org/sdr/IPXA2025100717233.md): Seal Depressor · cracked · Oct 6, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > AFT CARGO DOOR AFT SEAL DEPRESSOR RETAINER IS CRACKED AT THE UPPER CORNEER SPLICE
- [SDR IPXA2025092420680](https://openairdocs.org/sdr/IPXA2025092420680.md): Floor Panel · broken · Sep 24, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLIGHT COMPARTMENT FLOOR PANEL 211EP HAS 2 INSERT NUTS BROKEN.INSTALLED 2 INSERT NUTS IN FLIGHT COMPARTMENT FLOOR PANEL 211EP IAW A300-600 SRM 51-40-23
- [SDR IPXA2025102411698](https://openairdocs.org/sdr/IPXA2025102411698.md): Panel · pulled · Sep 15, 2025 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO PANEL 143DF HAS TWO INSERTS PULLED THROUGH. 33-051. REMOVED 2EA DAMAGED INSERTS AND REPLACED WITH 2EA NEW INSERTS P/N SL618-3CM BATCH # 0004404298 IAW EO # A300-5320-16407.
- [SDR IPXA2025092911698](https://openairdocs.org/sdr/IPXA2025092911698.md): Floor Panel · damaged · Sep 15, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO PANEL 143DF HAS TWO INSERTS PULLED THROUGH. 33-051 JOB COMPLETE. AUDIT COMPLETE.
- [SDR IPXA2025091972305](https://openairdocs.org/sdr/IPXA2025091972305.md): Adapter · broken · Sep 12, 2025 · N174UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, CLS ADAPTER AT RH SIDE JUST IN FRONT OF REDLINE MARKER NR 1 BROKEN. REMOVED CLS ADAPTER DAMAGE AT THE RT SIDE. FR20 IAW AIRBUS SRM 51-40-21-001. INSTALLED ADAPTER CLS, AT MAIN CARGO DECK, FLOOR STRUCTURE FR20 Y1954. IAW SRM 51-40-21-001.
- [SDR IPXA2025090647468](https://openairdocs.org/sdr/IPXA2025090647468.md): Floor Panel · delaminated · Sep 6, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > MCD FLOOR PANEL 231WG IS BADLY DELAMINATED. MCD FLOOR PANEL 231 WG IAW SREO-16407-REQ001 ((APPX B).PANEL INSTALLATION IS CONTROLLED ON TASK CARD T3F18E006XTN7.
- [SDR IPXA2025092009730](https://openairdocs.org/sdr/IPXA2025092009730.md): Bracket · cracked · Sep 4, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > RIGHT A/C PACKS CONICAL BELLCRANK BRACKET CRACKED. REMOVED BRACKET AT STR-RT A/C PACKS IAW SRM 5I-40-21. INSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025092340743](https://openairdocs.org/sdr/IPXA2025092340743.md): Fitting · gouged · Aug 30, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > LARGE VISIBLE GOUGE NOTED IN HOLE A AT 5 O'CLOCK DIRECTION. REAMED RH HOLE "A" TO 1ST OVERSIZE THROUGH ALL 5 LAYERS I.A.W EO-68606-JIC002 STEP 24 AND SRM 51-40-40. ACCOMPLISH THE REPAIR PER EO-95176-REQ1 AND EA 300-5710-27-A4116.
- [SDR IPXA2025083041546](https://openairdocs.org/sdr/IPXA2025083041546.md): Floor Panel · broken · Aug 30, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 231MJ IS BROKEN. FABRICATED MCD FLOOR PANEL 231MJ IAW SREO-16407-REQ001 ((APPX B). VERIFIED PANEL INSTALLATION IS CONTROLLED ON TASK CARD T3F18E006XTN7. JOB COMPLETE.
- [SDR IPXA2025083041834](https://openairdocs.org/sdr/IPXA2025083041834.md): Floor Panel · broken · Aug 30, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 231LG IS BROKEN. PANEL INSTALLATION IS CONTROLLED ON TASK CARD T3F18E006XTN7. JOB COMPLETE. IAW A300-600 AMM 53-10-23/401.
- [SDR IPXA2025110629932](https://openairdocs.org/sdr/IPXA2025110629932.md): Panel · damaged · Aug 29, 2025 · N174UP · Airbus A300F4622R · Passenger/Crew Doors
  > ***SUPPLEMENTAL SDR*** FAULT: STR-831- CREW DOOR PANEL 831EZ HAS A BENT LATCH HOOK. REMOVED AND REPLACED LATCH HOOK ON PANEL 831EZ IAW A-300 SRM 51-40-20-001.
- [SDR IPXA2025093016175](https://openairdocs.org/sdr/IPXA2025093016175.md): Access Panel · corroded · Aug 29, 2025 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON, ACCESS PANEL 414ER, AROUND OF THE HOLE FASTENER HAS CORROSION. REMOVED CORROSION ON ACCESS PANEL 414ER, AROUND OF THE HOLE FASTENER IAW A300-600 SRM 51-74-10 AFTER REWORK THE MEASURES WAS FOLLOWING ORIGINAL THICKNESS 0.080" LOSS MATERIAL 0.020" RE
- [SDR IPXA2025090200932](https://openairdocs.org/sdr/IPXA2025090200932.md): Hook · bent · Aug 29, 2025 · N174UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR PANEL 831EZ HAS A BENT LATCH HOOK.
- [SDR IPXA2025100212155](https://openairdocs.org/sdr/IPXA2025100212155.md): Bracket · cracked · Aug 28, 2025 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO, FR 38.2, STRAP SUPPORT PANEL, HAS SIX BRACKETS CRACKED. REMOVED THE BRACKETS AT THE FWD CARGO FR38.2 STRAP SUPPORT PANEL BULK. IAW SRM 51-40-21-001. RESTORED SURFACE IN NEW BRACKETS 6EA IAW A300 SRM 51-21-10. FABRICATED NEW BRACKETS IAW GMM 09.08
- [SDR IPXA2025082809049](https://openairdocs.org/sdr/IPXA2025082809049.md): Floor Panel · broken · Aug 28, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 252LG IS BROKEN. MCD FLOOR PANEL 252 LG IAW SREO-16407-REQ001 (APPX B) / PANEL INSTALLATION IS CONTROLLED ON TASK CARD T3F18E006XTN5.
- [SDR IPXA2025092070520](https://openairdocs.org/sdr/IPXA2025092070520.md): Floor Panel · damaged · Aug 26, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132QG HAS DAMAGED EDGES ON UNDERSIDE OF PANEL DOT 55-104. REPAIRED FLOOR PANEL IAW A300-600 SREO-42722-REQ001. PANEL 132QG TO BE INSTALLED ON TASK CARD T3F18E006XTNH. JOB COMPLETE.
- [SDR IPXA2025092648850](https://openairdocs.org/sdr/IPXA2025092648850.md): Hinge · cracked · Aug 25, 2025 · N174UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE HOLE 14F CRACK NOTED IN ALUMINUM LAYERS. REAMED HOLE 14F TO.261" IAW SRM 51-40-44. COMPLIED WITH EA 300-5236-27-A4122 REV-, STEP 19, PRELIMINARY 2. INSTALLED FASTENER AT HOLE 14F. RECEIVED FINAL DRAFT OF EA 300-5236-27-A4122 ACCOMPLISHED STEPS 1-2
- [SDR IPXA2025092651025](https://openairdocs.org/sdr/IPXA2025092651025.md): Frame · cracked · Aug 25, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT CENTER WING BOX CENTER SPAR AT FR44 CUTOUT DOUBLER RUN OUT RH ON I/B TOP HOLE. PERFORMED REAM HOLE 2 OVER (0.277) IN CENTER WING BOX SPAR AT FR 44 CUT-OUT DOUBLER RUN OUT RT ON INBD TOP HOLE PER SRM 51-40-40. ACCOMPLISSHED STEP 9 ON
- [SDR IPXA2025083038214](https://openairdocs.org/sdr/IPXA2025083038214.md): Strap · cracked · Aug 24, 2025 · N174UP · Airbus A300F4622R · Engine Thrust Reverser
  > NUMBER 1 ENG INBD THRUST REVERSER INTERNAL STRUCTURE, REAR UPPER FLANGE PLATE HAD A GOUGE. LOCATED AND DRILLED STRAP IAW SRM 51-40-40. INSTALLED NEW STRAP IAW SRM 51-40-21.
- [SDR IPXA2025092439192](https://openairdocs.org/sdr/IPXA2025092439192.md): Plate · deformed · Aug 24, 2025 · N174UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > ONE WEB PLATE DEFORMED AT RT WING INNER FLAP INTERNAL STRUCTURE BTWN RIB 23A & RIB 24B AND BTWN STGR 2.4 & STGR 2.5. IAW SRM 51-73-10-201 LENG OFF DAMAGE 0.100", FABRICATED NEW WEB PLATE IAW GMM 09.08.01.04 REV N:8.0. DRAWING 27-A579-60114. INSTALLED NEW WEB
- [SDR IPXA2025083139414](https://openairdocs.org/sdr/IPXA2025083139414.md): Barrier · corroded · Aug 24, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > L-SHAPED BARRIER RT SIDE BETWEEN FRAMES 19-20, Y953-Y1552 HAS CORROSION. REMOVED CORROSION IN SHAPED BARRIER AT FWD FACE OF RT FRAME 19-20 Y953-Y1552 IAW SRM 51-74-10. AFTER EVALUATE ON THE AREA 1 & AREA 3 IT WAS FOUND TO BE OUT OF LIMITS, ON AREA 2, AREA 4 &
- [SDR IPXA2025083028870](https://openairdocs.org/sdr/IPXA2025083028870.md): Web · cracked · Aug 23, 2025 · N174UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON AT RIB 3A UPPER SUPPORT HAD A CRACK. REMOVED DOOR PANEL SUPPORT STRUCTURE DAMAGED AT THE RIB A3 NR 1 PYLON IAW SRM 51-40-01-001. INSTALLED NR 1 PYLON AT RIB 3A UPPER SUPPORT IAW AMM 54-52-61/401.
- [SDR IPXA2025091125361](https://openairdocs.org/sdr/IPXA2025091125361.md): Floorbeam · corroded · Aug 23, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT FLOOR PANEL AREA, AT FR65 BETWEEN Y850 AND Y1470 FLOOR PANEL SUPPORT EXFOLIATED. FABRICATED AND REPARED REPAIR PARTS OF THE CROSSBEAM UPPER FRANGE AT AFT CARGO FR65 BTW Y850 AND Y1470. PROFILE EXTRUDED SECTION AND FILLER REPAIR. I.A.W AI
- [SDR IPXA2025100821478](https://openairdocs.org/sdr/IPXA2025100821478.md): Frame · cracked · Aug 23, 2025 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 2 ENG PYLON, UPPER SIDE, BETWEEN PANEL 423AL TO 423BL, SUPPORT ARC SHAPE FRAME HAS CRACKS. REMOVED SUPPORT UPPER SIDE IN RIBS 3 #2 ENG PYLON. AFTER FURTHER EVALUATIONS 02 CRACKS FOUND OUT OF LIMITS. IAW AIRBUS A300-600 SRM 54-52-51 PAG.2 FIG.1 AND SRM
- [SDR IPXA2025092713122](https://openairdocs.org/sdr/IPXA2025092713122.md): Angle · cracked · Aug 22, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > ONE ANGLE BRACKET CRACKED AT THE COCKPIT FLOOR SUPPORT STRUCTURE AT FR 10, Y-953. REMOVED ANGLE BRACKET IAW SRM 51-40-21 AT THE COCKPIT FLOOR SUPPORT STRUCTURE AT FR 10, Y-953. RECEIVED FROM FAB SHOP NEW PICKUP ANGLE P/N UPA 5361225120300. INSTALLED NEW PI
- [SDR IPXA2025091499931](https://openairdocs.org/sdr/IPXA2025091499931.md): Flap · corroded · Aug 22, 2025 · N174UP · Airbus A300F4622R · Trailing Edge Flaps
  > ***SUPPLEMENTAL SDR*** FAULT - STR, Z600, RH WING, O/B FLAP, UPPER SKIN, O/B SIDE, UNDER STATIC WICK HAS CORROSION. DOT 103-8. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94994-REQ1 AND VT-MAE EA 300-5754-27-A4128.
- [SDR IPXA2025091916219](https://openairdocs.org/sdr/IPXA2025091916219.md): Adapter · corroded · Aug 22, 2025 · N174UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > EVIDENCE OF CORROSION AROUND SEAT TRACK BY FR 27, Y450 TO Y0, (LT SIDE). REMOVED CORROSION 2EA AREAS AROUND SEATRACK BY FR27, Y450 TO Y0. INSTALLED NEW PART IAW A300-600, SRM 51-40-21.
- [SDR IPXA2025092916237](https://openairdocs.org/sdr/IPXA2025092916237.md): Seat Track · corroded · Aug 22, 2025 · N174UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > EVIDENCE OF CORROSION AROUND SEAT TRACK BY FR 26, Y450 TO Y0, (LH SIDE). FABRICATED NEW PART IAW GMM 09-08.INSTALLED NEW PART IAW SRM 51-40-21.
- [SDR IPXA2025091916217](https://openairdocs.org/sdr/IPXA2025091916217.md): Floor Panel · punctured · Aug 22, 2025 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 231XG HAS A PUNCTURE. REPAIRED SMALL SURFACE PUNCTURE I.A.W A300 SREO-42721-REQ001 (APPX A). JOB COMPLETE. REVIEWED
- [SDR IPXA2025092016159](https://openairdocs.org/sdr/IPXA2025092016159.md): Plate · broken · Aug 22, 2025 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > LEFT SIDE, BTW FR 38.1 AND FR 38.2 GUSSET PLATE IS BROKEN. INSTALLED NEW GUESSET PLATE L/H SIDE BTW FR 38.1 AND FR 38.2 IAW-SRM 51-40-20. REVIEWED
- [SDR IPXA2025091549931](https://openairdocs.org/sdr/IPXA2025091549931.md): Skin · corroded · Aug 22, 2025 · N174UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING, OTBD FLAP, UPPER SKIN, O/B SIDE, UNDER STATIC WICK HAS CORROSION. DOT 103-81 VERIFIED STEP #22 OF PRELIMINARY #1, E.A.#300-5754-27-A4128OF. VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. (T3F18E007E5EA)
- [SDR IPXA2025092689513](https://openairdocs.org/sdr/IPXA2025092689513.md): Fitting · cracked · Aug 21, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Structure
  > CRACK FOUND ON LT FR 40 UPPER SKIN LEVEL TENSION BOLT (BOTTOM HOLE) ACCOMPLISH REPEAT INSECTIONS PER SRI 57-10-24-2-001-00 FIRST INSPECTION AFTER 4200FC/9200FH (WHICH EVER COMES FIRST) METHOD IS WHICHEVER VALUE COMES FIRST. SUBSEQUENT INSPECTIONS AFTER 4200FC/
- [SDR IPXA2025092690143](https://openairdocs.org/sdr/IPXA2025092690143.md): Rib · cracked · Aug 21, 2025 · N174UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-95120-REQ1 AND VT-MAE EA 300-5750-27-A4111.
- [SDR IPXA2025083196649](https://openairdocs.org/sdr/IPXA2025083196649.md): Adapter · corroded · Aug 21, 2025 · N174UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE AT FR62, Y0 SEAT TRACK BASE HAS A CORROSION. RECEIVED CLS ADAPTER FROM FABRICATION P/N UPA53275455200 PO#PFB0000621 TRAVELER #T25/1831438. INSTALLED CLS (SEAT TRACK SUPPORT STRUCTURE). AT THE FR62, Y0.
- [SDR IPXA2025092997111](https://openairdocs.org/sdr/IPXA2025092997111.md): Seat Track · corroded · Aug 21, 2025 · N174UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE FR54 - FR 54.1, -Y450 SEAT TRACK UPPER SURFACE HAS LIGHT CORROSION. VERIFIED FINAL DRAFT OF EA# 300-5315-27-A4129 STEPS 1-3 ACCOMPLISHED WITHOUT DEVIATIONS. JOB COMPLETE.
- [SDR IPXA2025090996885](https://openairdocs.org/sdr/IPXA2025090996885.md): Adapter · corroded · Aug 21, 2025 · N174UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE AT FR76 BETWEEN Y1456 AND Y1959 SEAT TRACK HAS CORROSION. REMOVED ADAPTER CLS PER SRM 51-40-21. INSTALLED CLS ADAPTER MAIN DECK FLOOR STRUCTURE AT FR76 BETWEEN Y1456 AND Y1959 SEAT PER SRM 51-40-21.
- [SDR IPXA2025101457211](https://openairdocs.org/sdr/IPXA2025101457211.md): Support · cracked · Aug 19, 2025 · N174UP · Airbus A300F4622R · Engine Thrust Reverser
  > ENG NR 2 INBD THRUST REVERSER LOWER LATCHES COVER SUPPORT HAS A CRACK. CLEANED AREA AT ENG NR 2 INBD THRUST REVERSER LOWER LATCHES COVER SUPPORT IAW AMM 12-21-12. REMOVED LOWER LATCHES COVER SUPPORT IAW SRM 51-40-21. INSTALLED NEW LONGERON ON NR 2 INBD THR
- [SDR IPXA2025101357340](https://openairdocs.org/sdr/IPXA2025101357340.md): Angle · cracked · Aug 19, 2025 · N174UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > ENG NR 2 PYLON AFT FAIRING SUPPORT I/B AREA HAS A CRACK. REMOVED MEMBER ASSY-PICKUP P/N: A5451520600000 AT ENG #2 PYLON AFT FAIRING SUPPORT I/B AREA IAW SRM 51-40-21. RECEIVED WELDED MEMBER ASSY P/N: UPA545152415000 ON TRAVELER T25/1831545. INSTALLED MEMBER
- [SDR IPXA2025100951382](https://openairdocs.org/sdr/IPXA2025100951382.md): Splice · cracked · Aug 19, 2025 · N174UP · Airbus A300F4622R · Leading Edge Devices
  > LEFT WING KRUEGER FLAP INSIDE AREA, OTBD STRUCTURE HAS A CRACK, 1.00 INCH LONG,
- [SDR IPXA2025082531501](https://openairdocs.org/sdr/IPXA2025082531501.md): Skin · bent · Aug 18, 2025 · N174UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > NLG LEFT CUTOUT PANEL IS BENT AND HAS 2 CRACKS. INSTALLED NEW NLG LT CUTOUT PANEL IAW SRM 51-40-21.
- [SDR IPXA2025070235081](https://openairdocs.org/sdr/IPXA2025070235081.md): Light · inoperative · Jul 2, 2025 · N174UP · Airbus A300F4622R · Emergency Lighting
  > EXIT LIGHT INOP. EXIT SIGN LIGHTING WORKS NORMAL AT THIS TIME. OPS CHECK AMM 33-51-13/401
- [SDR IPXA2025070212307](https://openairdocs.org/sdr/IPXA2025070212307.md): Adc · faulted · Jul 1, 2025 · N174UP · Airbus A300F4622R · Air Data Computer
  > ATB, DURING CRUISE @FL300 NAV ADC-PRED W/S DET FAULT. ALSA WEATHER FAIL. TRIED TO RESET IW SYSTEM RESET TABLE\ AOM NO EFFECT. ATB R&R TRANSMITTER RECEIVER UNIT (8SQ) IAW AMM 34-41-51/401. PERFORMED WEATHER RADAR SYSTEM TEST IAW 34-41-00/501 AND PASSED. NO DEF
- [SDR IPXA2025070112307](https://openairdocs.org/sdr/IPXA2025070112307.md): Radar · faulted · Jul 1, 2025 · N174UP · Airbus A300F4622R · Weather Radar System
  > **SDR FILED OPEN** *** ATB *** DURING CRUISE @FL300 NAV ADC-PRED W/S DET FAULT. ALSA WEATHER FAIL. TRIED TO RESET IW SYSTEM RESET TABLE. AOM NO EFFECT. ATB
- [SDR IPXA2025060550402](https://openairdocs.org/sdr/IPXA2025060550402.md): Door · stuck · Jun 5, 2025 · N174UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW UNABLE TO OPEN CREW ENTRY DOOR AND DOOR JAMMED AND STUCK OPEN ABOUT 2 INCH OUTWARD.UNABLE TO OPEN AND CLOSED. SERVICED FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-14. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS MEL, PLACARD REMOVED.
- [SDR IPXA2024120541102](https://openairdocs.org/sdr/IPXA2024120541102.md): Sign · intermittent · Dec 5, 2024 · N174UP · Airbus A300F4622R · Emergency Lighting
  > EXIT SIGN OVER CREW DOOR FLICKERS ON AND OFF INTERMITTENTLY. CHECKED LIGH ASSEMBLY. FOUND BULBS LOOSE AND ADJUSTED, OPS CHECKS GOOD IAW AMM 33-51-13
- [SDR IPXA2024112699958](https://openairdocs.org/sdr/IPXA2024112699958.md): Slide · low pressure · Nov 26, 2024 · N174UP · Airbus A300F4622R · Escape Slide
  > CREW REPORTS L1 DOOR SLIDE PRESSURE LOW ACCOMPLISHED INSPECTION OF CREW DOOR ESCAPE SLIDE INFLATION RESERVOIR PRESSURE GAUGE PER AMM 25-61-20-601. FOUND INFLATION RESERVOIR PRESSURE GAUGE WHITE NEEDLE WITHIN THE LIMITS OF GREEN TEMPERATURE COMPENSATED MOVABLE

Next page: https://openairdocs.org/aircraft/N174UP/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 = 'N174UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N174UP/reports

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