# Service difficulty reports: N393UP

A list on [N393UP](https://openairdocs.org/aircraft/N393UP.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 2 · 52 reports

- [SDR IPXA2026102020598](https://openairdocs.org/sdr/IPXA2026102020598.md): Sign · inoperative · Oct 19, 2026 · N393UP · Boeing 767316 · Emergency Lighting
  > DURING PSM FOUND EMERGENCY EXIT SIGN NEXT TO ENTRY DOOR NOT ILLUMINATING FIM 33-51 FT 805 REV. 149 FOLLOWED, PRESSED TEST BUTTON ON BATTERY PACK, NO LIGHTS ILLUMINATING. BATTERY PACK REPLACED IAW AMM 33-51-07/201 REV, 149 AND EMERGENCY LIGHTS TESTED SATISFACTO
- [SDR IPXA2026101920598](https://openairdocs.org/sdr/IPXA2026101920598.md): Battery Pack · inoperative · Oct 19, 2026 · N393UP · Boeing 767316 · Emergency Lighting
  > DURING PSM FOUND EMERGENCY EXIT SIGN NEXT TO ENTRY DOOR NOT ILLUMINATING FIM 33-51 FT 805 REV. 149 FOLLOWED, PRESSED TEST BUTTON ON BATTERY PACK, NO LIGHTS ILLUMINATING. BATTERY PACK REPLACED IAW AMM 33-51-07/201 REV, 149 AND EMERGENCY LIGHTS TESTED SATISFACTO
- [SDR IPXA2026091744608](https://openairdocs.org/sdr/IPXA2026091744608.md): Housing · cracked · Sep 2, 2026 · N393UP · Boeing 767300 · Fuel Storage
  > ***MAJOR REPAIR*** FAULT - FOUND FUEL LEAK AT NO.2 SLAT OUTBD MAIN TRACK HOUSING DRAIN HOLE. ACCOMPLISHED THE REPAIR I.A.W UPS EO-98615-REQ1 REV1 AND BOEING DWG NO. 112T2001 SH 21 REV: D.
- [SDR IPXA2026082995025](https://openairdocs.org/sdr/IPXA2026082995025.md): Blowout Door · chafed · Aug 21, 2026 · N393UP · Boeing 767316 · Engine Thrust Reverser
  > CHAFED SKIN OF NR 1 ENG RT THRUST REVERSER LOWER BLOWOUT DOOR INNER L/E AREA. INSTALLED NEW BLOWOUT DOOR IAW SRM 51-40-02-0G, REV 132, & AIPC 78-31-51-03, REV 40, IPC 78-32-22, REV 96, & AMM 78-31-19-402-008, REV 149.
- [SDR IPXA2026082995720](https://openairdocs.org/sdr/IPXA2026082995720.md): Former · cracked · Aug 21, 2026 · N393UP · Boeing 767316 · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 456. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 132, DWG 114T2202, SH 1, REV D, AND SREO-57209-REQ001, REV 2.
- [SDR IPXA2026082994280](https://openairdocs.org/sdr/IPXA2026082994280.md): Longeron · chafed · Aug 21, 2026 · N393UP · Boeing 767316 · Nacelle/Pylon, Longeron/Stringer
  > CHAFED LONGERON, NR 1 ENG LT CORE COWL AFT LWR AREA. INSTALL A NEW LONGERON IAW SRM 51-40-02-0G, REV 132, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026082995671](https://openairdocs.org/sdr/IPXA2026082995671.md): Former · cracked · Aug 21, 2026 · N393UP · Boeing 767316 · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 499. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 132, & DWG 114T2511, SH 1, REV D, SREO-50900-REQ001, REV 2.
- [SDR IPXA2026091681129](https://openairdocs.org/sdr/IPXA2026091681129.md): Panel · worn · Aug 20, 2026 · N393UP · Boeing 767300 · Wing Main, Frame Structure
  > WORN - HOLE, RT WING NR 8 SLAT INBD SIDE LWR CLOSURE DOOR. (REPAIR). IAW SRM 57-43-01-2R-3 REFER TO SRM 51-70-08-0G-0 REV. 132 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE SIZE AND LOCATION ( L: 0.3", W: 0.2"
- [SDR IPXA2026090377741](https://openairdocs.org/sdr/IPXA2026090377741.md): Skin · debonded · Aug 20, 2026 · N393UP · Boeing 767316 · Wing, Plate/Skin
  > DEBONDED SKIN, INBD EDGE UPPER FACE OF LT WING T/E OTBD FLAP T/E SKIN, WBL 355. IAW SREO-70175-REQ001, REV 1, REMOVED THE CRACK AND CLEANED. MEASURE THE DAMAGE AREA L: 0.5", W: 0.01", 7" FROM TRAILING EDGE, AT INBD EDGE. BONDED THE REPAIR PLIES WITH RE
- [SDR IPXA2026082877723](https://openairdocs.org/sdr/IPXA2026082877723.md): Skin · dented · Aug 20, 2026 · N393UP · Boeing 767316 · Nacelle/Pylon, Plate/Skin
  > DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT DAMAGE AND CLEANED, MEASURE CUT OUT DIA 0.8", FROM FWD EDGE 27.5", AT 6 O'CLOCK ON INNER BARREL OF NR 2 ENG INLET COWL. BONDED THE SPACER WITH FILM ADHESIVE CURED AT 250 F FOR 2 HRS & FILLED
- [SDR IPXA2026082877089](https://openairdocs.org/sdr/IPXA2026082877089.md): Skin · debonded · Aug 20, 2026 · N393UP · Boeing 767316 · Trailing Edge Flaps
  > DEBONDED LOWER SKIN OF LT WING T/E OTBD FLAP T/E SKIN, WBL 366. IAW SRM 57-53-01-2R-1 REF SRM 51-70-07-0G-0, REV 132. PERFORMED A REPAIR IAW STEP 1. REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION(DIA:1", 33.5" FROM INBD EDGE,
- [SDR IPXA2026082877721](https://openairdocs.org/sdr/IPXA2026082877721.md): Skin · debonded · Aug 20, 2026 · N393UP · Boeing 767316 · Wing, Plate/Skin
  > DEBONDED LOWER SKIN OF LT WING T/E OTBD FLAP T/E SKIN WBL 380. IAW SRM 57-53-01-2R-1, REF SRM 51-70-07-0G-0, REV 132. PERFORMED A REPAIR IAW STEP 1. REMOVED THE DEBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:6",W:1", 11" FROM INBD E
- [SDR IPXA2026082577721](https://openairdocs.org/sdr/IPXA2026082577721.md): Skin · debonded · Aug 20, 2026 · N393UP · Boeing 767300 · Trailing Edge Flaps
  > DISBOND - SKIN, LOWER SKIN OF L/H WING T/E OUTBD FLAP T/E SKIN WBL 380 (REPAIR) CORRECT THE TYPO IN STEP 1: 1.I.A.W. 767-300 SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.132 PERFORM REPAIR AS BELOW STEP: 1. REMOVE THE DISBOND MATERIALS AND CLEAN. 1.2 MEA
- [SDR IPXA2026082577089](https://openairdocs.org/sdr/IPXA2026082577089.md): Skin · debonded · Aug 20, 2026 · N393UP · Boeing 767300 · Trailing Edge Flaps
  > DISBOND - SKIN, LOWER OF L/H WING T/E OUTBD FLAP T/E SKIN, WBL 366 (REPAIR) CORRECT THE TYPO IN STEP 1: 1.I.A.W. 767-300 SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.132 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DISBOND MATERIALS AND CLEAN. 1.2 MEASU
- [SDR IPXA2026082577741](https://openairdocs.org/sdr/IPXA2026082577741.md): Skin · debonded · Aug 20, 2026 · N393UP · Boeing 767300 · Trailing Edge Flaps
  > DISBOND - SKIN, INBD EDGE UPPER FACE OF L/H WING T/E OUTBD FLAP T/E SKIN, WBL 355 (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 6" AROUND HEATED AREA,PER 767 NDT MANUAL PART 1 51-01-01 REV:144 RESULT: NO DEFECT WAS FOUND
- [SDR IPXA2026082961141](https://openairdocs.org/sdr/IPXA2026082961141.md): Former · cracked · Aug 19, 2026 · N393UP · Boeing 767316 · Wing Main, Frame Structure
  > CRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 648.6. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 132, DWG 114T2513, SH 1, REV D, & SREO-50900-REQ001, REV 2.
- [SDR IPXA2026082634262](https://openairdocs.org/sdr/IPXA2026082634262.md): Seat Track · cracked · Aug 18, 2026 · N393UP · Boeing 767316 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND FIRST OFFICER SEAT TRACK ASSY CRACK AT FORWARD INBOARD. IAW AMM 25-11-01-822-095-001, REV 149. REPLACED THE SEAT TRACK.
- [SDR IPXA2026080873740](https://openairdocs.org/sdr/IPXA2026080873740.md): Pad · damaged · Aug 7, 2026 · N393UP · Boeing 767316 · Wing Main, Frame Structure
  > COMPOSITE AREA SURROUNDING RT WING FIXED LEADING EDGE MOST OTBD BEARING PAD IS CRACKED & CHIPPED AWAY. IAW AMM 51-21-10-307-020, REV 149, REPAINTED REWORK AREA. CONDITION CHECKED NORMAL.
- [SDR IPXA2026062535966](https://openairdocs.org/sdr/IPXA2026062535966.md): Latch · inoperative · Jun 24, 2026 · N393UP · Boeing 767316 · Passenger/Crew Doors
  > MAIN ENTRY DOOR LATCH UNABLE TO LOCK. PERFORMED OPERATIONAL TEST OF CREW ENTRY DOOR REF AMM 52-11-00. OPS CHECKED GOOD. DOOR CLOSES AND LOCKS AS INTENDED
- [SDR IPXA2026083005141](https://openairdocs.org/sdr/IPXA2026083005141.md): Seal Depressor · damaged · Jun 10, 2026 · N393UP · Boeing 767316 · Cargo/Baggage Doors
  > RAMP REPORTED DAMAGE TO MCD AFT SEAL DEPRESSOR. INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-02-0G, REV 132 AND IAI DWG 368-53-00-95301, ISSUE AV.
- [SDR IPXA2026052858550](https://openairdocs.org/sdr/IPXA2026052858550.md): Skin · damaged · Mar 24, 2026 · N393UP · Boeing 767316 · Leading Edge Devices
  > MAJOR REPAIR, OVERSIZE RIVET HOLES, IN SLAT INSERT FITTING AND SLAT LEADING EDGE RIB ATTACH FASTENERS NR 9 SLAT ALL STEPS OF EO-96917-REQ7 C/W.
- [SDR IPXA2025100720177](https://openairdocs.org/sdr/IPXA2025100720177.md): Gearbox · stuck · Oct 6, 2025 · N393UP · Boeing 767* · Leading Edge Slat Actuator
  > WHILE EXTENDING FLAPS FROM UP TO 1, RECEIVED LE FLAP ASYM EICAS MSG AND LEADINGEDGE DISCRETE LIGHT. INSTALLED INBOARD AND OUTBOARD ROTARY ACTUATORS AND OFFSET GEARBOX IAW. AMM 27-81-20 PB 201 REV. 146. AFTER INSTALLATION OF LEADING EDGE SLAT #8, #9 AND #10 AN
- [SDR IPXA2025031292106](https://openairdocs.org/sdr/IPXA2025031292106.md): Knob · out of adjust · Mar 12, 2025 · N393UP · Boeing 767316 · Doppler System
  > CREW REPORTS THAT THE TILT KNOB POSITION DID NOT MATCH WITH THE INDICATION ON THE NAV DISPLAY. TILT KNOB ADJUSTED IAW AMM 34-43-02 PB401 REV.144. AND TESTED IAW AMM 34-43-00 PB501 REV.144. FOUND SATIS.
- [SDR IPXA2024120432892](https://openairdocs.org/sdr/IPXA2024120432892.md): Idg · failed · Dec 4, 2024 · N393UP · Boeing 767316 · AC Generator-Alternator
  > ATB L GEN OFF DURING TAKEOFF ROLL. RAN CHECKLIST, RESULTED IN MOMENTARY GEN OPERATION BEFORE FAILING AGAIN. ATB REPLACED JAW AMM 24-22-02 PB 401 SATIS
- [SDR IPXA2024082938616](https://openairdocs.org/sdr/IPXA2024082938616.md): None · none · Aug 19, 2024 · N393UP · Boeing 767316 · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR
- [SDR IPXA2024081938616](https://openairdocs.org/sdr/IPXA2024081938616.md): Drain · none · Aug 19, 2024 · N393UP · Boeing 767316 · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPEN
- [SDR IPXA2024082516569](https://openairdocs.org/sdr/IPXA2024082516569.md): Floor Panel · damaged · Aug 17, 2024 · N393UP · Boeing 767316 · Fuselage Floor Panel
  > MAJOR REPAIR, DAMAGE FOUND M/D FLOOR PNL DAMAGE P/N:371-53-13-C4218-103 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-13-C4218-103
- [SDR IPXA2024082516559](https://openairdocs.org/sdr/IPXA2024082516559.md): Floor Panel · damaged · Aug 17, 2024 · N393UP · Boeing 767316 · Fuselage Floor Panel
  > MAJOR REPAIR, DAMAGE - FOUND M/D FLOOR PNL DAMAGE P/N:371-53-15-C6405-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-15-C6405-101.
- [SDR IPXA2024082516575](https://openairdocs.org/sdr/IPXA2024082516575.md): Floor Panel · damaged · Aug 17, 2024 · N393UP · Boeing 767316 · Fuselage Floor Panel
  > MAJOR REPAIR, DAMAGE, FOUND M/D FLOOR PNL DAMAGE P/N: 368-53-00-95626-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-00-95626-101
- [SDR IPXA2024082996283](https://openairdocs.org/sdr/IPXA2024082996283.md): Pump · cracked · Aug 16, 2024 · N393UP · Boeing 767316 · Fuel Boost Pump
  > *** SUPPLEMENTAL SDR *** FAULT - CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV 143 REPLACE THE R/H WING AUX FUEL PUMP PNLNO.631AB. 2.CONDITION CHECK NORMAL. 3.IPC VERIFIED AND SERVICEABLE TA
- [SDR IPXA2024082993754](https://openairdocs.org/sdr/IPXA2024082993754.md): Handle · broken · Aug 16, 2024 · N393UP · Boeing 767316 · Passenger/Crew Doors
  > FOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE 1. I.A.W AIPC 52-11-25-13-144 REV.28 TO REMOVE FWD ENTRY DOOR HANDLE. 2. I.A.W AIPC 52-11-25-13-144 REV.28 TO INSTALL NEW FWD ENTRY DOOR HANDLE. 3. I.A.W AMM TASK 52-11-00-715-128 REV.143 TO DO OPERATIONAL TEST
- [SDR IPXA2024081693754](https://openairdocs.org/sdr/IPXA2024081693754.md): Bearing · broken · Aug 16, 2024 · N393UP · Boeing 767316 · Passenger/Crew Doors
  > FOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE OK TO WORK
- [SDR IPXA2024081696283](https://openairdocs.org/sdr/IPXA2024081696283.md): Access Panel · cracked · Aug 16, 2024 · N393UP · Boeing 767316 · Wing, Plate/Skin
  > CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE)
- [SDR IPXA2024090674434](https://openairdocs.org/sdr/IPXA2024090674434.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Fuselage Main, Plate/Skin
  > SKIN DENTED, RT FUSELAGE TAIL SECTION BS 1915.1 - 1923.5. MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.4" DEPTH(Y)=0.006" AND A/Y = 66 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126
- [SDR IPXA2024090674300](https://openairdocs.org/sdr/IPXA2024090674300.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Fuselage Main, Plate/Skin
  > DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-36R (EVALUATE) MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.6" DEPTH(Y)=0.007" AND A/Y = 85 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126
- [SDR IPXA2024082977067](https://openairdocs.org/sdr/IPXA2024082977067.md): Skin · cracked · Aug 15, 2024 · N393UP · Boeing 767316 · Wing, Plate/Skin
  > *** SUPPLEMENTAL SDR *** FAULT - CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR) INSTALLED L/H WING LEADING EDGE UPPER FIX PANEL I.A.W SRM 51-40-02-0G REV.126 AND BOEING DWG 114T2230 SH1 REV.D AND 114T2510 SH1 REV.E AND 114T21
- [SDR IPXA2024082977129](https://openairdocs.org/sdr/IPXA2024082977129.md): Skin · cracked · Aug 15, 2024 · N393UP · Boeing 767316 · Leading Edge Devices
  > CRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL, NEAR INBD TRACK (REPAIR) INSTALLED LEFT WING NO.3 SLAT CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.126
- [SDR IPXA2024082976940](https://openairdocs.org/sdr/IPXA2024082976940.md): Skin · cracked · Aug 15, 2024 · N393UP · Boeing 767316 · Leading Edge Devices
  > CRACK - SKIN, LOWER FACE OF L/H WING NO.6 SLAT MID LINK LOWER DOOR (REPAIR) 1.I.A.W AMM 57-41-59-404-009 REV 143 INSTALLED THE LEFT WING NO.6 SLAT MIDDLE LINK DOOR, AND PERFORMED THE DOOR ADJUSTMENT WAS SATISFIED. 2.CONDITION CHECK NORMAL.
- [SDR IPXA2024082975427](https://openairdocs.org/sdr/IPXA2024082975427.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Auxiliary Power Unit (APU) Doors
  > *** SUPPLEMENTAL SDR *** FAULT - DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) 1. MEASURED THE DENT DIMENSION LENGTH=0.8" WIDTH(A)=0.5" DEPTH(Y)=0.005" AND A/Y = 100 FOUND TO BE IN LIMIT PER SRM 52-40-01-1A-6 FIGURE 101 DETAIL IV REV.126 2. SUB
- [SDR IPXA2024082577039](https://openairdocs.org/sdr/IPXA2024082577039.md): Floor Panel · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1197+132~1329, LBL11~RBL11, P/N:368-53-16-94477-127 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-94
- [SDR IPXA2024082577009](https://openairdocs.org/sdr/IPXA2024082577009.md): Floor Panel · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1121.1~1197, LBL 11 ~ RBL 11, P/N:368-53-16-94477-109 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-
- [SDR IPXA2024081577129](https://openairdocs.org/sdr/IPXA2024081577129.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Wing, Plate/Skin
  > CRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL, NEAR INBD TRACK (REPAIR)
- [SDR IPXA2024081577067](https://openairdocs.org/sdr/IPXA2024081577067.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Wing, Plate/Skin
  > CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR)
- [SDR IPXA2024081574422](https://openairdocs.org/sdr/IPXA2024081574422.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Fuselage Main, Plate/Skin
  > DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1788 S-38R~S-39R (EVALUATE) OK TO WORK
- [SDR IPXA2024081574300](https://openairdocs.org/sdr/IPXA2024081574300.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316F · Fuselage Main, Plate/Skin
  > DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-38R ~ S39R (EVALUATE) OK TO WORK
- [SDR IPXA2024081574434](https://openairdocs.org/sdr/IPXA2024081574434.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316F · Fuselage Main, Plate/Skin
  > DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1915.1 - 1923.5 (EVALUATE) OK TO WORK
- [SDR IPXA2024081575427](https://openairdocs.org/sdr/IPXA2024081575427.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316 · Auxiliary Power Unit (APU) Doors
  > DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) OK TO WORK
- [SDR IPXA2024052987755](https://openairdocs.org/sdr/IPXA2024052987755.md): A/C Pack · odor · May 28, 2024 · N393UP · Boeing 767316 · Cabin Cooling System
  > STRONG ACRID OIL SMELL WITH PACKS ON WHILE USING BLEED AIR FROM APU ALSO NOTICED FILM ON INSIDE OF WINDOW AND CAUSED EYE IRRITATION AFTER LONG APU RUN WITH BOTH PACKS ON, THE SMOKE SMELL DISAPPEARED. OPS TEST PERFROMED IAW AMM 21-00-21-102-030, REV: 142.
- [SDR IPXA2024032194772](https://openairdocs.org/sdr/IPXA2024032194772.md): Valve · warning message · Mar 21, 2024 · N393UP · Boeing 767300 · Engine Bleed Air System
  > *DIVERSION* R ENG PRV STATUS MESSAGE ON TAKEOFF #2 ENG PRV MANUAL WRENCHING ACCOMPLISHED AND VERIFIED TO BE HARD TO WRENCH AND WITH STUCK POSITION IN THE MIDDLE. THEREFORE #2 ENG PRV REPLACED AS PER AMM 36-11-18/401 REV.141 OPS AND LEAK TEST FOUND SATIS.
- [SDR IPXA2023111611610](https://openairdocs.org/sdr/IPXA2023111611610.md): Adc · faulted · Nov 16, 2023 · N393UP · Boeing 767300 · Air Data Computer
  > ATB, IN FLIGHT ALT DISAGREE? EICAS MESSAGE DISPLAYED. 1ST OFFICER AIR DATA DETERMINED TO BE AT FAULT, ALT AIR DATA SELECTED PERFORMED T/S ON PITOT & STATIC SYS AS PREVIOUS TESTS SHOWED AN ALTITUDE DIFFRENCE OF 100 FEET BETWEEN CAPT AND F/O SIDE. CHECKED ALL CO

Next page: https://openairdocs.org/aircraft/N393UP/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 = 'N393UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N393UP/reports

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