# Service difficulty reports: Boeing 767-316

A list on [Boeing 767-316](https://openairdocs.org/model/boeing-767-316.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 10 · 453 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 ABXA20260927437](https://openairdocs.org/sdr/ABXA20260927437.md): Brake · faulted · Sep 27, 2026 · N227CY · Boeing 767316 · Landing Gear Brake System
  > DURING TAKEOFF, FROM UIO CREW REJECTED TAKEOFF (RTO) WITH HIGH ENERGY STOP, BLOWING ALL 8 TIRES A/C ROLLED ON BLOWN TIRES AND CONTINUED TAXIING TO PARKING SPOT. COMPLETED HIGH ENERGY STOP OR HEAT DAMAGE CONDITIONAL INSPECTION FOR ALL TIRE DEFLATED CONDIT
- [SDR ABXA20260926436](https://openairdocs.org/sdr/ABXA20260926436.md): Door · unlocked · Sep 26, 2026 · N227CY · Boeing 767316 · Cargo/Baggage Doors
  > ON ENGINE START, MAIN CARGO DOOR LIGHT & HORN SOUNDED. CREW RETURNED TO THE GATE (BTB). MTC FOUND MAIN DECK CARGO DOOR CLOSED BUT NOT LOCKED. CLOSED AND LOCKED MAIN DECK CARGO DOOR IAW AMM 52-32-00. DOOR CLOSED & LOCKED PROPERLY. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260921429](https://openairdocs.org/sdr/ABXA20260921429.md): Warning Light · intermittent · Sep 21, 2026 · N227CY · Boeing 767316 · Door Warning System
  > MASTER WARNING PARTIAL TONE AND DISCRETE WARNING LIGHT INTERMITTENTLEY FLASHING ON AND OFF VERIFIED TO BE MCD DOOR IND. DEFERRED IAW MEL 52-30-3-4 MAINT PROC C/W (DEFERRED MDC DOOR INDICATION) PLACARD INSTALLED. REINSPECT BEFORE EACH FLIGHT. A/C RETURNED TO SE
- [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 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 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 ABXA20260808353](https://openairdocs.org/sdr/ABXA20260808353.md): Warning Message · false activation · Aug 8, 2026 · N227CY · Boeing 767316 · Fire Detection
  > R ENG FIRE LOOP 2 STATUS MSG. PERFORMED ENGINE FIRE DETECTION SYSTEM OPS TEST PER AMM 26-11-00. OPS TEST PASSED, MSG CLEARED, A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE.
- [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 ABXA20260803346](https://openairdocs.org/sdr/ABXA20260803346.md): Generator · malfunctioned · Aug 3, 2026 · N227CY · Boeing 767316 · AC Generator-Alternator
  > LEFT GEN OFF WITH LEFT BUS TIE LIGHT / ISLN LIGHT ON WHEN POWER ADVANCED FOR TAKEOFF. A/C ABORTED TAKE OFF (ATO) AND RETURNED TO GATE (BTB). MTC DEFERRED LH GEN IAW ABX MEL 24-00-1-2. GENERATOR DISCONNECTED MX PROCEDURES ACCOMPLISHED. PLACARDS INSTALLED. A/C R
- [SDR ABXA20260726336](https://openairdocs.org/sdr/ABXA20260726336.md): Circuit Breaker · tripped · Jul 26, 2026 · N227CY · Boeing 767316 · Smoke Detection
  > FIRE DET. CARGO DC CB OPEN. RESET FIRE DET CARGO DC CB, PERFORMED AFLOT DET. TEST NO ISSUES NOTED, SYSTEM OK AT THIS TIME, IAW AMM 26-11-00 AND 20-60-01 AIRCRAFT REMAINS ETOPS 180. A/C RETURNED TO SERVICE.
- [SDR ABXA20260718324](https://openairdocs.org/sdr/ABXA20260718324.md): Relay · malfunctioned · Jul 18, 2026 · N227CY · Boeing 767316 · Trailing Edge Flap Control System
  > DURING TAXI FLAP SLAT DISAGREE - TE FLAP DISAGREE APPEARED, A/C RETURNED TO THE GATE (BTB),MTX GROUNDED A/C AND BEGAN TO TROUBLE SHOOT, FOUND RELAY K623 BAD FLAP BYPASS STAYING IN ALTERNATE MODE. REPLACED RELAY. ALL FLAP FUNCTIONS AND INDICATIONS NORMAL. R
- [SDR ABXA20260628289](https://openairdocs.org/sdr/ABXA20260628289.md): Module · defective · Jun 28, 2026 · N227CY · Boeing 767316 · Hydraulic Power Accumulator, Main
  > DURING TAXI, CENTER HYD SYSTEM PRESSURE 1070 PSI WITH BOTH ENGINES RUNNING, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. TROUBLE SHOT AND REMOVED AND REPLACED CENTER PRESSURE AND CASE DRAIN MODULE IAW B767 AMM 29-11-19, OPS TEST GOOD, NO LEAKS NOTED AT THI
- [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 ABXA20260603239](https://openairdocs.org/sdr/ABXA20260603239.md): Fire Loop · faulted · Jun 3, 2026 · N227CY · Boeing 767316 · Smoke Detection
  > DURING MAINTENANCE PREFLIGHT,RH FIRE LP 2 EICAS MSG APPEARED, MTX GROUNDED A/C AND DEFERRED RH LP 2 LOOP FOR DEPARTURE IAW MEL 26-11-1-1, PLACARD INSTALLED, MBCB 06/13/26, A/C RELEASED NO ETOPS, PLACARD ROTATED.AND RETURNED A/C TO SERVICE.
- [SDR ABXA20260525223](https://openairdocs.org/sdr/ABXA20260525223.md): Sensor · out of adjust · May 25, 2026 · N227CY · Boeing 767316 · Leading Edge Slat Position Indicating System
  > EICAS MSG LE FLAP ASYM FLAP INDICATOR STOPPED BETWEEN 1 AND UP. A/C THEN PERFORMED AIR TURN BACK (ATB) TO FIELD AND LANDED. MTX GROUNDED A/C AND TROUBLESHOT AND FOUND #4 SLAT SENSOR "S279" OUT OF ADJUSTMENT. PLACED SENSOR BACK TO CORRECT INDUCTANCE RANGE, REF
- [SDR ABXA20260515201](https://openairdocs.org/sdr/ABXA20260515201.md): Warning Light · illuminated · May 15, 2026 · N227CY · Boeing 767316 · Smoke Detection
  > MAIN DECK CARGO FIRE PANEL POSITION A2 HAS FAULT LIGHT ILLUMINATED. MTX GROUNDED A/C MTX C/W AFOLTS TEST IAW B767 AMM 26-10-00 OPS CHECK GOOD NO MSG AT THIS TIME. AND RETURNED A/C TO SERVICE.
- [SDR ABXA20260510192](https://openairdocs.org/sdr/ABXA20260510192.md): Proximity Sensor · defective · May 10, 2026 · N227CY · Boeing 767316 · Fuel Controlling System
  > DURING PUSH. WHEN WE STARTED THE RIGHT ENGINE, "R ENG CONTROL" AND "R ENG MODE EEC EICAS" SHOWED.AND A/C RETURNED TO GATE (BTB),MTX GROUNDED A/C AND TROUBLESHOT TO LEFT GEAR TILT SENSOR "S267" FAULTED. REMOVED & REPLACED THE SENSOR, REF B767 AMM 32-09-02. ALL
- [SDR IPXA2026042684022](https://openairdocs.org/sdr/IPXA2026042684022.md): Timer · faulted · Apr 25, 2026 · N395UP · Boeing 767316 · Fuel Boost Pump
  > FOUND FAULTY TIME DELAY K5 FOR R FWD BOOST PUMP REPLACED THE TIME DELAY K5 RELAY IAW SWPM:20-81-11 REV.38 AND FOUND OPS TEST OF RT FWD FUEL PUMP SATISFACTORY IAW AMM:28-22-00/501 REV.148 CONFIRMED ALL PARTS AND TOOLS REMOVED FROM ACFT.
- [SDR ABXA20260416167](https://openairdocs.org/sdr/ABXA20260416167.md): Starter · defective · Apr 16, 2026 · N227CY · Boeing 767316 · Engine Starter
  > ON TAXI OUT, RT ENGINE DID NOT TURN ON. TRIED MANUAL START, BUT NOTHING. A/C DID A GROUND RETURN (BTB). MAINTENANCE FOUND STARTER LEAKING. REMOVED AND REPLACED RH ENG STARTER PER BAMM 80-11-01. OPS CK NORMAL ON RUN UP. PER BAMM 71-00-00. ACFT REMAINS NO E
- [SDR ABXA20260415166](https://openairdocs.org/sdr/ABXA20260415166.md): Starter · faulted · Apr 15, 2026 · N227CY · Boeing 767316 · Engine Starter
  > ON TAXI OUT AND WHILE ATTEMPTING TO START THE RIGHT ENGINE THE R STARTER EICAS W/ ASSOC VALVE DISCRETE LIGHT ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). MTC DEFERRED R ENG START VALVE IAW B767 MEL 80-00-2-1 PLACARDS INSTALLED. MX PROCEDURES C/W. MBCB 04/25/26
- [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 ABXA202603132100](https://openairdocs.org/sdr/ABXA202603132100.md): Wire · detached · Mar 12, 2026 · N227CY · Boeing 767316 · Pneumatic System Wiring
  > IN CRUISE, RT STRUT DUCT LEAK AND RT ENG BLEED OFF LIGHTS ILLUMINATED. CREW DID AN AIR TURN BACK TO SDF. (ATB). MAINTENANCE RETERMINATED WIRE W 376-454 R-18 AT TS 238. PERFORMED GRND IDLE RUN. OPS CHECK GOOD. NO LIGHTS, NO MESSAGES. WORK DONE IAW RSWPM 20-30
- [SDR ABXA202603110093](https://openairdocs.org/sdr/ABXA202603110093.md): Smoke Detector · no test · Mar 10, 2026 · N227CY · Boeing 767316 · Smoke Detection
  > CREW REPORTED FWD EQUIP SMOKE LIGHT MESSAGE DID NOT TEST. MAINTENANCE REMOVED AND REPLACED FWD LOWER CARGO SMOKE DETECTOR IAW B767 AMM 26-16-01. OPS TEST GOOD. A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE.
- [SDR IPXA2026022511384](https://openairdocs.org/sdr/IPXA2026022511384.md): Flap · none · Feb 14, 2026 · N395UP · Boeing 767316 · Trailing Edge Flaps
  > DOUBLER, REPAIR DOUBLER NOT EXIST ON MAPPING, RIGHT WING INBD FLAP AFT FLAP UPPER SURFACE, WBL 265 (AGING INSPECTION (NO.4734) (EVALUATE). ACCOMPLISH REPAIR PER 767-300 SRM 57-53-01-2R-1, 51-70-10-2R-0 AND 51-70-10-2R-4 REV. 130, WITHOUT DEVIATION. REVIEW CO
- [SDR IPXA2026022411434](https://openairdocs.org/sdr/IPXA2026022411434.md): Floorbeam · cracked · Feb 14, 2026 · N395UP · Boeing 767316 · Fuselage Main, Floor Beam
  > CRACKED BRACKET, MAIN DECK FLOOR BEAM TO FUSELAGE BRACKET, STA 917 S-21L (AGING INSPECTION) (NO.4736) (REPLACE). INSTALL REPAIR PART -T01 STRINGER CLIP AS SHOWN IN FIGURE 2 AND PER IAI DWG 371-53-00-C4181-001 REQUIREMENTS. ACCOMPLISHED REPAIR I.A.W EO-96668-R
- [SDR IPXA2026022470882](https://openairdocs.org/sdr/IPXA2026022470882.md): Rib · cracked · Feb 12, 2026 · N395UP · Boeing 767316 · Wing, Rib/Bulkhead
  > CRACKED FITTING, RT WING OTBD L/E RIB LES 600, NOSE INTERIOR. INSTALLED A FABRICATED RIB IAW SRM 51-40-02-0G, REV 130, AND DWG 114T2606, SHEET 1, REV E, DWG 114T2601, SHEET 1, REV B, DWG 114T2301, SHEET 3, REV C, DWG 114T2250, SHEET 1, REV A, DWG 114T224
- [SDR IPXA2026022546988](https://openairdocs.org/sdr/IPXA2026022546988.md): Splice · corroded · Feb 11, 2026 · N395UP · Boeing 767316 · Fuselage Main, Keel
  > CORROSION-SPLICE TEE, SEC45 LOWER FUSELAGE KEEL AREA BS 910, RBL 9.5 INNER SURFACE (AGING INSPECTION) (NO.4701). INSTALLED NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV. 130 AND DWG 145T8629 SH. 2 REV. A.
- [SDR IPXA2026022024931](https://openairdocs.org/sdr/IPXA2026022024931.md): Skin · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Passenger/Crew Doors
  > MAJOR REPAIR, CRACKED FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED THE DOORWAY LINING IAW AMM 52-11-02-404-025, REV. 80.
- [SDR IPXA2026022024904](https://openairdocs.org/sdr/IPXA2026022024904.md): Skin Panel · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Fuselage Main, Plate/Skin
  > CRACK, FWD ENTRY DOOR RH AFT LOWER CORNER SKIN. (REPAIR). ACCOMPLISH THE REPAIR I.A.W EO-87307-REQ8 REV2 AND SRM 53-10-01-2R-1 REV.130 AND EGAT WORK SHEET NO.60098. REVIEW COMPLETE.
- [SDR IPXA2026030322790](https://openairdocs.org/sdr/IPXA2026030322790.md): Depressor · deformed · Feb 10, 2026 · N395UP · Boeing 767316 · Fuselage Main, Structure
  > DEFORMED SILL, MAIN DECK CARGO DOOR CUTOUT AFT EDGE. FABRICATE IAW DWG 368-53-00-95379, SH 2, REV F, PL REV M, & GMM-MTX, 9.08, REV 14. INSTALLED THE FABRICATED PART IAW SRM 51-40-02-0G, REV 130, AND DWG 368-53-00-95301, SH 6, ISSUE AV.
- [SDR IPXA2026030223168](https://openairdocs.org/sdr/IPXA2026030223168.md): Channel · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 1 PYLON AFT FAIRING PANEL 437DB INNER OTBD SIDE CHANNEL. INSTALLED A NEW BULKHEAD ANGLE IAW SRM 51-40-02-0G, REV 130 AND DWG 313T2362, SHT 4, REV B.
- [SDR IPXA2026022523383](https://openairdocs.org/sdr/IPXA2026022523383.md): Bracket · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 2 PYLON INTERNAL RESERVOIR HYD TUBE SUPPORT BRACKET AT R/H SIDE UPPER HINGE BEAM AREA. (REPLACE). IAW SRM 51-40-02-0G REV. 130 AND AIPC 54-51-53-18 REV. 36 INSTALLED NEW BRACKET.
- [SDR IPXA2026022410668](https://openairdocs.org/sdr/IPXA2026022410668.md): Channel · cracked · Feb 9, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD INBD SIDE CHANNEL. (REPLACE). INSTALLED NEW CHANNEL I.A.W SRM 51-40-02-0G REV. 130 AND BOEING DWG NO. 313T3380 SH. 5 REV. H AND 313T2362 SH. 4 REV. B. REVIEW COMPLETE.
- [SDR IPXA2026022510717](https://openairdocs.org/sdr/IPXA2026022510717.md): Channel · cracked · Feb 9, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 2 PYLON AFTER FAIRING PANEL 447DB INNER OUTBOARD CHANNEL CRACK. (REPLACE). INSTALLED NEW CHANNEL I.A.W SRM 51-40-02-0G REV. 130 AND BOEING DWG NO. 313T2362 SH. 4 REV. B. REVIEW COMPLETE.
- [SDR IPXA2026020900534](https://openairdocs.org/sdr/IPXA2026020900534.md): Wedge · debonded · Feb 8, 2026 · N395UP · Boeing 767316 · Trailing Edge Flaps
  > FAULT - RIGHT WING INBOARD AFT FLAP WEDGE, INBOARD SIDE UPPER SKIN DISBOND (REPAIR). ACCOMPLISH REPAIR PER 767-300 SRM 57-53-01-2R-1, 51-70-10-2R-0 AND 51-70-10-2R-4 REV. 130, WITHOUT DEVIATION. REVIEW COMPLETE.
- [SDR IPXA2026022899828](https://openairdocs.org/sdr/IPXA2026022899828.md): Beam · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon, Main Frame
  > CRACKED BEAM, NR 1 PYLON AFT FAIRING INNER INBD SIDE LWR BEAM. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 130, SB 767-54-0109, REV 1, DWG 313T2303, SHT 25, REV A, DWG 313T2303, SHT 27, REV A, DWG 313T2303, SHT 28, REV A, DWG 313T2303, SHT 29, REV A,
- [SDR IPXA2026022400346](https://openairdocs.org/sdr/IPXA2026022400346.md): Support Bracket · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, NR 2 PYLON AFTER FAIRING INNER VANE TUBE SUPPORT NR 1 SUPPORT BRACKET (REPLACE). INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 130 AND DWG 272T0182 SH. 1 REV. A.
- [SDR IPXA2026022400341](https://openairdocs.org/sdr/IPXA2026022400341.md): Support Bracket · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 2 PYLON AFTER FAIRING INNER VANE TUBE SUPPORT NR 2 SUPPORT BRACKET (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV. 130 AND DWG 272T0182 SH. 1 REV. A.
- [SDR IPXA2026022099584](https://openairdocs.org/sdr/IPXA2026022099584.md): Former · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Leading Edge Devices
  > CRACKED FORMER, LT WING L/E NR 4 SLAT INBD DOOR LINK INBD CURTAIN SUPPORT WS 564 (REPLACE) REVIEW COMPLETE.
- [SDR IPXA2026022099451](https://openairdocs.org/sdr/IPXA2026022099451.md): Former · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Leading Edge Devices
  > CRACKED SUPPORT, LT WING L/E NO.5 SLAT OUTBD DOOR LINK CURTAIN OUTBD SUPPORT, OSS 499 (REPLACE) REVIEW COMPLETE.

Next page: https://openairdocs.org/model/boeing-767-316/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 aircraft_model_key = '767316'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-316/reports

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