# Service difficulty reports: N317UP

A list on [N317UP](https://openairdocs.org/aircraft/N317UP.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 · 152 reports

- [SDR IPXA2026070872957](https://openairdocs.org/sdr/IPXA2026070872957.md): Support Beam · corroded · Jun 26, 2026 · N317UP · Boeing 76734AF · Wing, Landing Gear Attach Fittings
  > LEFT MLG SUPPORT BEAM ASSY OUTER BUSHING OF AFT TRUNNION BEARING HAS CORROSION ON LOWER EDGE. INSTALLED OUTER BUSHING P/N 113T1108-33SAAU AT LH MLG BEAM ASSY IAW CMM 57-54-13 REPAIR 2-1. ACCOMPLISHED REPAIR PER EO-98083-REQ1 AND EA 767-5754-01-B0785, REV IR,
- [SDR IPXA2026070774298](https://openairdocs.org/sdr/IPXA2026070774298.md): Fitting · corroded · Jun 26, 2026 · N317UP · Boeing 76734AF · Wing, Landing Gear Attach Fittings
  > RIGHT WING REAR SPAR, OUTBOARD SUPPORT OF TRUNNION BEARING HAS CORROSION ON O/B AND LOWER SPOT FACE, FLL-003, ACCOMPLISHED INSTRUCTIONS PER EO-97989-REQ1 AND EA 767-5751-01-B0774 REV IR. NO FURTHER ACTION IS REQUIRED.
- [SDR IPXA2026033071018](https://openairdocs.org/sdr/IPXA2026033071018.md): Web · corroded · Mar 20, 2026 · N317UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CORROSION, AFT CARGO BALL PANEL AND FLOOR STRUCTURE FAYING SURFACE STA 1197+132 ~ 1219 RBL 40 ~ 50. (AGING A/C INSPECTION) (NO. 2868) (EVALUATE) INSTALL FAB WEB AND FASTENERS I.A.W 51-40-02-0G REV. 94 AND BOEING DWG NO: 146T5001 SHEET 14 REV. D; 146T5001 SHE
- [SDR IPXA2026032975575](https://openairdocs.org/sdr/IPXA2026032975575.md): Plate · cracked · Mar 20, 2026 · N317UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND THE PLATE ON SIDE GUIDE RAIL WITH CRACK DAMAGE AT BS 1219, LEFT SIDE IN AFT CARGO COMPARTMENT. INSTALLED NEW TIE PLATE IAW SRM 51-40-02-0G, REV 94, & AIPC 25-53-15-21, REV 141.
- [SDR IPXA2026032776354](https://openairdocs.org/sdr/IPXA2026032776354.md): Receptacle · worn · Mar 20, 2026 · N317UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > WORN RECEPTACLE, NR 2 ENGINE NOSE COWL EXTERNAL MID LOWER OUTER SKIN AT 6 O'CLOCK. INSTALLED A NEW RECEPTACLE IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-11-16 REV. 54.
- [SDR IPXA2026032978429](https://openairdocs.org/sdr/IPXA2026032978429.md): Depressor · chafed · Mar 20, 2026 · N317UP · Boeing 76734AF · Fuselage Main, Structure
  > CHAFING & DEFORM - FRAME, MAIN DECK CARGO DOOR CUTOUT AREA & AFT SIDE. INSTALL NUTPLATES ON NEW DEPRESSOR IAW SRM 51-40-02-0G REV. 94 AND DWG 143T1008, SHT, 11 REV. - & 143T8414 SH 1 REV. G AND 143T8414 SH 2 REV. A..
- [SDR IPXA2026032675990](https://openairdocs.org/sdr/IPXA2026032675990.md): Skin · cracked · Mar 20, 2026 · N317UP · Boeing 76734AF · Trailing Edge Flaps
  > CRACKED SKIN, LT WING FLAP FAIRING NR 3 AFT EDGE. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" HEATED AREA, PER NDT MANUAL PART 1 51-01-01 REV:143. NO DEFECT WAS FOUND. IAW AMM 20-11-00-910-802 REV.147 INSTALLED THE SCREWS.
- [SDR IPXA2026033051174](https://openairdocs.org/sdr/IPXA2026033051174.md): Bracket · corroded · Mar 19, 2026 · N317UP · Boeing 76734AF · Wing Main, Frame Structure
  > GOUGED BRACKET, LT WING T/E LOWER SURFACE WBL 289. ACCOMPLISHED GOUGE AND CORROSION DAMAGE REPAIR IAW EO-96933-REQ1, REV 1, & SRM 51-40-02-0G, REV 94, DWG 113T1944, SHT 2, REV A, & DWG 113T1551, SHT 1, REV E.
- [SDR IPXA2026032052387](https://openairdocs.org/sdr/IPXA2026032052387.md): Repair · debonded · Mar 19, 2026 · N317UP · Boeing 76734AF · Leading Edge Devices
  > MAJOR REPAIR, DEBONDED, PREVIOUS REPAIR, L/H WING NO.5 SLAT UPPER SURFACE LES 440. CUT OUT THE DAMAGE MATERIALS AND CLEAN, MEASURE THE CUTOUT SIZE (L:5.75", W:5.25", 38" FROM INBD EDGE AT AFT EDGE OF THE LT WING NR 5 SLAT UPPER SURFACE LES 440) IAW SRM 57-43
- [SDR IPXA2026033158453](https://openairdocs.org/sdr/IPXA2026033158453.md): Door · damaged · Mar 19, 2026 · N317UP · Boeing 76734AF · Emergency Equipment
  > THE DESCENT DEVICE CONTAINER DOOR IS CRACKED. REPAIRED THE LID ASSY IAW EO-96902-REQ1, REV 2.
- [SDR IPXA2026032252574](https://openairdocs.org/sdr/IPXA2026032252574.md): Repair · debonded · Mar 19, 2026 · N317UP · Boeing 76734AF · Leading Edge Devices
  > DEBONDED PREVIOUS REPAIR, LT WING NR 5 SLAT UPPER SURFACE LES 500. INSTALL THE EXTERNAL DOUBLER WITH FILM ADHESIVE IAW SRM 51-70-10-2R-0 PARAGRAPH 10 & 18 REV. 94. ACCOMPLISH THE REPAIR PER SRM (REV 94) 57-43-02-2R-1 REPAIR 1, AND 51-70-10-2R-4 REPAIR 4.
- [SDR IPXA2026032456367](https://openairdocs.org/sdr/IPXA2026032456367.md): Angle · cracked · Mar 19, 2026 · N317UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND ANGLE CRACK AT ENTRY DOOR SCUFF PLATE. INSTALLED NEW CLIP ASSY I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 141T8310 SH. 4 REV. H.
- [SDR IPXA2026032053114](https://openairdocs.org/sdr/IPXA2026032053114.md): Bracket · chafed · Mar 19, 2026 · N317UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22, REV 94.
- [SDR IPXA2026032056184](https://openairdocs.org/sdr/IPXA2026032056184.md): Bracket · chafed · Mar 19, 2026 · N317UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENGINE RT THRUST REVERSER FWD LOWER CLOSEOUT INNER TRAILING EDGE. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 94 AND IPC 78-32-22 REV. 94.
- [SDR IPXA2026032057534](https://openairdocs.org/sdr/IPXA2026032057534.md): Bracket · cracked · Mar 19, 2026 · N317UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED SUPPORT, RT WING L/E INBD PANEL 611KB, TORQUE SUPPORT LES 281. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND DWG 114T1240, SH 4, REV D.
- [SDR IPXA2026032058453](https://openairdocs.org/sdr/IPXA2026032058453.md): Door · cracked · Mar 19, 2026 · N317UP · Boeing 76734AF · Emergency Equipment
  > THE DESCENT DEVICE CONTAINER DOOR IS CRACKED. (REPLACE) OK TO WORK.
- [SDR IPXA2026032831078](https://openairdocs.org/sdr/IPXA2026032831078.md): Angle · damaged · Mar 18, 2026 · N317UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > DAMAGED ANGLE, NR 2 NACELLE AFT SKIRT FAIRING INNER RT, 4TH HINGE FITTING.. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3310, SHEET 1, REV L.
- [SDR IPXA2026032331814](https://openairdocs.org/sdr/IPXA2026032331814.md): Clamp · broken · Mar 18, 2026 · N317UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > BROKEN CLAMP, NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, & DWG 313T3349, SH 2, REV B.
- [SDR IPXA2026032332844](https://openairdocs.org/sdr/IPXA2026032332844.md): Beam · cracked · Mar 18, 2026 · N317UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED BEAM, NR 2 NACELLE AFT LOWER FAIRING RT UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 94 AND DWG 313T2380, SH. 10, REV K, 313T2380, SH 9, REV G, 313T2380, SH 22, REV F, & SERVICE BULLENTIN 767-54-010
- [SDR IPXA2026032331943](https://openairdocs.org/sdr/IPXA2026032331943.md): Angle · cracked · Mar 18, 2026 · N317UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 2 PYLON AFT LOWER FAIRING INNER FWD BULKHEAD LT REAR MID. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026032010352](https://openairdocs.org/sdr/IPXA2026032010352.md): Hinge Fitting · cracked · Mar 17, 2026 · N317UP · Boeing 76734AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING T/E NR 10 SPOILER INBD LWR FITTING. REPLACED DAMAGED FITTING IAW SRM 51-40-02-0G, REV 94, & DWG 112T1000, SH 14, REV B, 113T1422, SH 1, REV D, 112T1001, SH 45, REV -, 113T1653, SH 1, REV J, & 113TT1678, SH 1, REV A.
- [SDR IPXA2026082593903](https://openairdocs.org/sdr/IPXA2026082593903.md): Pawl · worn · Mar 16, 2026 · N317UP · Boeing 76734AF · Passenger/Crew Doors
  > HE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL I.A.W AMM 52-11-26-004-001 REV.147 AND AMM 52-11-26-404-003 REV.147.TORQUE SCREW TO 35 IN-LB.
- [SDR IPXA2026032591928](https://openairdocs.org/sdr/IPXA2026032591928.md): Skin · cracked · Mar 16, 2026 · N317UP · Boeing 76734AF · Passenger/Crew Doors
  > CRACKED FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. ACCOMPLISH THE REPAIR IAW EO-87307-REQ7, REV 2, & SRM 53-10-01-2R-1, REV 130, AND EGAT WORK SHEET 60160.
- [SDR IPXA2026031793903](https://openairdocs.org/sdr/IPXA2026031793903.md): Pawl · worn · Mar 16, 2026 · N317UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. OPEN
- [SDR IPXA2026020667134](https://openairdocs.org/sdr/IPXA2026020667134.md): Landing Gear · faulted · Jan 31, 2026 · N317UP · Boeing 76734AF · Landing Gear Retraction/Extension System
  > EMERGENCY DECLARED, NOSE GEAR WOULD NOT COME DOWN AFTER !0 MIN WITH GEAR HANDLE IN THE DOWN POSITION MANUALLY DEPLOYED GEAR EXT PER QRH. CENTER HYD SYSTEM ADP FILTER MODULE WAS FOUND TO BE BYPASSING NOT ALLOWING CENTER HYD SYSTEM ADP TO OPERATE PROPERLY, CENT
- [SDR IPXA2026020558217](https://openairdocs.org/sdr/IPXA2026020558217.md): Wire · chafed · Jan 30, 2026 · N317UP · Boeing 76734AF · Door System Wiring
  > LEFT FWD ENTRY DOOR EICAS MSG ON PUSHBACK FOUND WIRE ON SWITCH S194 CHAFED. REMOVED AND REPLACED CREW ENTRY DOOR SWITCH S194 IAW B767 AMM 52-71-01 AND SWPM 20-30-12. OPS CHECK GOOD. THIS CLEARS DEFERRAL. REVERSED DMP. PLACARD REMOVED
- [SDR IPXA2026013058217](https://openairdocs.org/sdr/IPXA2026013058217.md): Warning Message · illuminated · Jan 30, 2026 · N317UP · Boeing 76734AF · Door Warning System
  > LEFT FWD ENTRY DOOR EICAS MESSAGE ON PUSH BACK, DMP C/W IAW MEL 52-71-1-1A.
- [SDR IPXA2025073083108](https://openairdocs.org/sdr/IPXA2025073083108.md): Window · cracked · Jul 29, 2025 · N317UP · Boeing 76734AF · Flight Compartment Windows
  > DIVERSION, L1 WINDOW CRACKED. REPLACED WINDSHIELD IAW AMM 56-11-01-404-017 REV 145. LEAK AND OPS CHECKED SATIS.
- [SDR IPXA2025032162167](https://openairdocs.org/sdr/IPXA2025032162167.md): Light · inoperative · Mar 20, 2025 · N317UP · Boeing 76734AF · Emergency Lighting
  > FOUND EMERGENCY LIGHT INOP. FOUND BATTERY PACK DRAINED, R/R EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-51-07/201. OPS TEST SATIS.
- [SDR IPXA2025031479934](https://openairdocs.org/sdr/IPXA2025031479934.md): Warning Message · false activation · Mar 11, 2025 · N317UP · Boeing 76734AF · Windshield/Door Rain/Ice Removal
  > EICAS L SIDE WINDOW. PERFORMED QRH PROCEDURE AND LIGHT EXTINGUISHED OPS CONT'D NORMAL PERFORMED BITE TEST PER FIM 30-41 FAULT TREE 804, NO FAULT NOTED. AIRCRAFT OK FOR SERVICE
- [SDR IPXA2024040886820](https://openairdocs.org/sdr/IPXA2024040886820.md): Hinge · deformed · Mar 27, 2024 · N317UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM I.A.W AMM 52-12-02-404-025 REV.141 INSTALL DOORWAY LINING. I.A.W AMM 20-10-13-964-001 REV.141 REPLACE DECAL. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024040287451](https://openairdocs.org/sdr/IPXA2024040287451.md): Angle · cracked · Mar 27, 2024 · N317UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACK - ANGLE BULK CARGO COMPARTMENT NEAR STA 1578 LBL 60 (REPLACE) 1.I.A.W AMM 53-01-06-400-801 REV.141 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL<BR>2.I.A.W AMM 25-59-01-404-019 REV.141 INSTALL MAIN DECK CARGO DADO PANEL AND CONDITION CHE
- [SDR IPXA2024032786820](https://openairdocs.org/sdr/IPXA2024032786820.md): Hinge · deformed · Mar 27, 2024 · N317UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE) OKAY TO WORK
- [SDR IPXA2024032853897](https://openairdocs.org/sdr/IPXA2024032853897.md): None · none · Mar 25, 2024 · N317UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR.
- [SDR IPXA2024032653856](https://openairdocs.org/sdr/IPXA2024032653856.md): Stiffener · cracked · Mar 25, 2024 · N317UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > STIFFENER CENTER WING FRONT SPAR CRACK IN STIFFENER AT STA 785.9 LBL55(REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 57-10-10-2R-2 REV.88 AND EGAT WORK SHEET NO.40286 AND UPS SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1
- [SDR IPXA2024032653897](https://openairdocs.org/sdr/IPXA2024032653897.md): None · none · Mar 25, 2024 · N317UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2024032653813](https://openairdocs.org/sdr/IPXA2024032653813.md): Skin · cracked · Mar 25, 2024 · N317UP · Boeing 76734AF · Leading Edge Devices
  > CRACK - SKIN, FWD LOWER FACE OF L/H WING NO.5 SLAT L/E NOSE SKIN, NEAR OUTBD TRACK AREA OSS 492.953.(REPAIR) REPAIR DAMAGE AREA I.A.W SRM 57-43-01-2R-2 REPAIR 2 REV.88 AND WORK SHEET NO.40287. JOB COMPLETED.
- [SDR IPXA2024022287752](https://openairdocs.org/sdr/IPXA2024022287752.md): Window · cracked · Feb 21, 2024 · N317UP · Boeing 76734AF · Flight Compartment Windows
  > L2 WINDOW HAS CRACK IN LOWER AFT CORNER. FLIGHT CREW FOUND PRIOR TO PRE FLIGHT. C/W REMAINING STEPS OF #2 L/H SLIDING WINDOW INSTALL MM 56-11-02.
- [SDR IPXA2022040380794](https://openairdocs.org/sdr/IPXA2022040380794.md): None · failed · Apr 3, 2022 · N317UP · Boeing 76734AF · Aircraft Fuel Distribution System
  > INSPECTION TYPE:NA**ATB** LEFT AFT FUEL PUMP FAILED 50 MINS AFTER TAKEOFF. CB POPPED. LEFT FORWARD FUEL PUMP FAILED 1:30 AFTER TAKEOFF. CB POPPED.LEFT AFT FUEL BOOST PUMP REPLACED IAW AMM 28-22-03 PB 401 REV 135.04. FUEL PUMP TESTED IAW AMM 28-22-00 PB 501. RE
- [SDR IPXA2022032280362](https://openairdocs.org/sdr/IPXA2022032280362.md): Skin · corroded · Mar 14, 2022 · N317UP · Boeing 76734AF · Cargo/Baggage Doors
  > INSPECTION TYPE:C13CORROSION ON INNER SKIN OF BULK CARGO DOOR AFT LOWER CORNER AREA AT STA 1457.REPAIR I.A.W 767-300F SRM 52-30-01-1A DETAIL VII,REV.82.01.
- [SDR IPXA2022030979915](https://openairdocs.org/sdr/IPXA2022030979915.md): Door · none · Mar 8, 2022 · N317UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:NAENTRY DOOR CAPTURE LEVER CAN NOT BE CLOSED FROM INSIDE CABIN, ONLY FROMEXTERIOR BY MECHANIC-WX WERE ABLE TO CLOSE IT FROM INSIDE W/MUCH DIFFICULTY HOWEVER BUT IT NEEDS TO BE TROUBLE SHOTLUBED LOWER DOOR MECHANISM AS REQUIRED OPS TEST OK ALL W
- [SDR IPXA2021050268878](https://openairdocs.org/sdr/IPXA2021050268878.md): Lamp · inoperative · May 2, 2021 · N317UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/AOUTSIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED OUTSIDE EMERGENCY LIGHT I/A/W AMM 33-51-16 OPS CHECK GOOD
- [SDR IPXA2021021165580](https://openairdocs.org/sdr/IPXA2021021165580.md): Proximity Switch · malfunctioned · Feb 11, 2021 · N317UP · Boeing 76734AF · Landing Gear Position and Warning
  > INSPECTION TYPE:N/A**ATB - SUPPLEMENTAL SDR - NO EMERG DECLARED - NO EMERG EQUIP USED - LANDED W/OUT INCIDENT** STATUS MESSAGE LANDING GEAR MONITOR. FOUND RT NOSE GEAR SYS 1 @ FAULT TRANSFERRED TO MEL/DMI M-735398 PER MEL 32-61-2-1 ACCOMPLISHED DMP 32-61-2-1
- [SDR IPXA2020122963918](https://openairdocs.org/sdr/IPXA2020122963918.md): Warning Message · false activation · Dec 28, 2020 · N317UP · Boeing 76734AF · Airfoil Anti/De-ice System
  > INSPECTION TYPE: N/A, DIVERSION, NO EMERGENCY DECLARED. DURING ARRIVAL BOTH "LT & RT ENGINE AI VALVE" MESSAGES OCCURED. MESSAGES CLEARED BY THEMSELVES BUT RE-APPEARED. DIVERTER DENVER TO PHOENIX DUE TO ICING IN DENVER TERMINAL AREA. T/S PER FIM 30-11-00-99
- [SDR IPXA2020080328542](https://openairdocs.org/sdr/IPXA2020080328542.md): Skin · damaged · Aug 2, 2020 · N317UP · Boeing 76734AF · Elevator, Plate/Skin
  > LEFT OTBD ELEVATOR UPPER SKIN DAMAGED 25.25", OTBD AND 10.25" FWD OF T/E. REPAIRED IAW B767-5520-77296.
- [SDR IPXA2020031853259](https://openairdocs.org/sdr/IPXA2020031853259.md): Skin · cracked · Mar 6, 2020 · N317UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C12CRACK ON L/E SKIN OF #8 SLAT NEAR OSS 592.95.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.76.01
- [SDR IPXA2020031853258](https://openairdocs.org/sdr/IPXA2020031853258.md): Skin · cracked · Mar 6, 2020 · N317UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C12CRACK ON L/E SKIN OF #4 SLAT NEAR OSS 607.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.76.01
- [SDR IPXA2020031853257](https://openairdocs.org/sdr/IPXA2020031853257.md): Skin · cracked · Mar 6, 2020 · N317UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C12CRACK ON L/E SKIN OF #9 SLAT NEAR OSS 572.55.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.76.01
- [SDR IPXA2020031853291](https://openairdocs.org/sdr/IPXA2020031853291.md): Stiffener · cracked · Mar 6, 2020 · N317UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-12) ON STA 785.9, RBL 33REPAIR I.A.W 767-300F SRM 5710-10-2R-2 REPAIR 2 REV.76.01, UPS EO B767-5740-58151-B, BOEING SRID: 4-4743157524 AND UPS EO B767-5710-75851-A
- [SDR IPXA2020031853290](https://openairdocs.org/sdr/IPXA2020031853290.md): Stiffener · cracked · Mar 6, 2020 · N317UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-11) ON STA 785.9, LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01, UPS EO B767-5740-58151-B, BOEING SRID: 4-4743157524 AND UPS EO B767-5710-75851-I

Next page: https://openairdocs.org/aircraft/N317UP/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 = 'N317UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N317UP/reports

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