# Service difficulty reports: Boeing 767-34AF

A list on [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 126 · 6,281 reports

- [SDR IPXA2026102276179](https://openairdocs.org/sdr/IPXA2026102276179.md): Lock Mechanism · faulted · Oct 22, 2026 · N327UP · Boeing 76734AF · Fixed Inner Doors
  > CREW REPORTS RIGID BARRIER DOOR UNABLE TO OPEN ON PREFLIGHT. PRIMARY LATCH LOCKING MECHANISM FAULTY. PRM ISO VALVE C/B K-3 AT P-33 OPENED AND COLLARED TO SHUT OFF AIR FLOW INTO THE PRM.
- [SDR IPXA2026102133469](https://openairdocs.org/sdr/IPXA2026102133469.md): Floor Panel · damaged · Oct 20, 2026 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE,
- [SDR IPXA2026102108780](https://openairdocs.org/sdr/IPXA2026102108780.md): Floor Panel · damaged · Oct 18, 2026 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE. IAW AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.149 REMOVED MAIN DECK CARGO HANDLING AND G.V.I CHECK NORMAL.IAW AMM 53-01-06-000-801 REV.149, REMOVED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2026101806238](https://openairdocs.org/sdr/IPXA2026101806238.md): Skin · punctured · Oct 18, 2026 · N351UP · Boeing 76734AF · Leading Edge Devices
  > DURING WALKAROUND, FOUND A PUNCTURE AT SLAT NR 10 (WS 624). SLAT CRACKED AT SEVERAL SPOTS, NUMEROUS RIVETS SHEARED. R/R SLAT #10 (STATION 624) IAW MM 27-81-02-024. ACCOMPLISHED OPS TEST PER MM 27-81-02/501 TEST FAIL. DUE TO NO SLAT TARGETS. S296,S310 SENSOR TA
- [SDR IPXA2026101456665](https://openairdocs.org/sdr/IPXA2026101456665.md): Adc · malfunctioned · Oct 14, 2026 · N328UP · Boeing 76734AF · Airspeed/Mach Indicator
  > EMERGENCY DECLARED, IN CRUISE EXPERIENCED AIRSPEED UNRELIABLE SITUATION PER QRH CHECKLIST WE DETERMINED THE LEFT SIDE WAS UNRELIABLE. DUE TO NON SPECIFIC FIM TASK, USED FAULT CODE INDEX WITH CODE 34 12 77 01 REV 149, REPL L ADC IAW AMM 34-12-01/401 REV 149,
- [SDR IPXA2026101442976](https://openairdocs.org/sdr/IPXA2026101442976.md): Flap System · faulted · Oct 14, 2026 · N323UP · Boeing 76734AF · Trailing Edge Flaps
  > AIR TURN BACK, EMERGENCY DECLARED. AFTER TAKEOFF ON FLAP RETRACTION EICAS MESSAGE LE SLAT ASYMMETRY. FOLLOWED QRH PROCEDURE COULD NOT RETRACT SLAT. RETURNED SDF.
- [SDR IPXA2026101325515](https://openairdocs.org/sdr/IPXA2026101325515.md): Controller · faulted · Oct 13, 2026 · N303UP · Boeing 76734AF · Windshield/Door Rain/Ice Removal
  > FO`S R2 WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED LT FWD AND RT SIDE WINDOW HEAT CONTROLLER UNIT (M191) IAW AMM 30-41-01/401. BITE TEST PASSED IAW B767 AMM 30-41-01-404-007. REVERSED DMP, AND REMOVED PLACARD.
- [SDR IPXA2026101092858](https://openairdocs.org/sdr/IPXA2026101092858.md): Life Raft · partial deploy · Oct 10, 2026 · N325UP · Boeing 76734AF · Life Raft
  > LIFE RAFT IN STOWAGE COMPARTMENT PARTIALLY DEPLOYED. REPLACED LIFE RAFT REF MM 25-62-01/401
- [SDR IPXA2026102268685](https://openairdocs.org/sdr/IPXA2026102268685.md): Skin · damaged · Oct 9, 2026 · N322UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > MAJOR REPAIR, PANEL AFT OF 321D RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 7.5€? FROM BOTTOM & 12€? FROM LEADING EDGE. PERFORMED NDT/UT FOR THE BONDED REPAIR & 8 INCHES FROM WHERE THE EDGES OF THE HEAT BLANKET, IAW NDT MANUAL PART 1 51-01-
- [SDR IPXA2026102268850](https://openairdocs.org/sdr/IPXA2026102268850.md): Skin · damaged · Oct 9, 2026 · N322UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > MAJOR REPAIR, PANEL AFT OF 321C RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 43€? FROM TOP & 14€? FROM TRAILING EDGE. SEE ATTACHED PICTURE. PERFORMED NDT/UT FOR THE BONDED REPAIR & 8 INCHES FROM WHERE THE EDGES OF THE HEAT BLANKET, I.A.W. 767
- [SDR IPXA2026100856727](https://openairdocs.org/sdr/IPXA2026100856727.md): Skin · debonded · Oct 2, 2026 · N354UP · Boeing 76734AF · Trailing Edge Flaps
  > FAULT - DISBOND - END CAP, R/H WING T/E OUTBD FLAP INBD. MEASURE THE DAMAGE AREA (L:1.5", W:0.1", D:2PLIES, 7" FROM AFT EDGE, AT INBD EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W UPS SREO-70175-R
- [SDR IPXA2026100857298](https://openairdocs.org/sdr/IPXA2026100857298.md): Skin · cracked · Oct 2, 2026 · N354UP · Boeing 76734AF · Trailing Edge Flaps
  > FAULT - CRACK - SKIN, R/H WING T/E INBD MAIN FLAP INBD UPPER. (REPAIR). MEASURE THE DAMAGE AREA (DIA:1", 16.5" FROM INBD EDGE, 3.5" FROM AFT EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F
- [SDR IPXA2026100553573](https://openairdocs.org/sdr/IPXA2026100553573.md): Former · broken · Oct 2, 2026 · N354UP · Boeing 76734AF · Wing Main, Frame Structure
  > BROKEN FORMER, LT WING OUTBD L/E FOLDING NOSE INNER SIDE AT OSS 441.60, ADJACENT NR 5 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 96. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 96, DWG 114T2241, SH 4, REV -, AND SREO-54290-REQ1, R
- [SDR IPXA2026100560445](https://openairdocs.org/sdr/IPXA2026100560445.md): Lens · missing · Oct 2, 2026 · N353UP · Boeing 76734AF · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT PANEL -LIGHT INDICATION MISSING LENS, REPLACED LENS IN REF WITH AMM 33-16-02 OPS CK NORMAL
- [SDR IPXA2026100259603](https://openairdocs.org/sdr/IPXA2026100259603.md): Door Latch · binding · Oct 2, 2026 · N329UP · Boeing 76734AF · Passenger/Crew Doors
  > ENTRY DOOR SECURE LATCH IS VERY HARD TO CLOSE /LATCH. LUBRICATED CREW ENTRY DOOR SECURE LATCH PER AMM 12-21-18/301.OPS CHECK OF CREW DOOR OK.
- [SDR IPXA2026100503114](https://openairdocs.org/sdr/IPXA2026100503114.md): Skin · dented · Sep 30, 2026 · N354UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > FAULT - DENT - SKIN, NO.1 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.2", 18.2" FROM L/E, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR
- [SDR IPXA2026100503125](https://openairdocs.org/sdr/IPXA2026100503125.md): Skin · dented · Sep 30, 2026 · N354UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > FAULT - DENT - SKIN, NO.1 ENG NOSE COWL INLET AT 3 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.25", 20.5" FROM L/E, AT 3 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR
- [SDR IPXA2026100603239](https://openairdocs.org/sdr/IPXA2026100603239.md): Skin · dented · Sep 30, 2026 · N354UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > FAULT - DENT - SKIN, NO.2 ENG NOSE COWL INNER BARREL AT 8 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.3", 8.2" FROM T/E, AT 8 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1
- [SDR IPXA2026100603252](https://openairdocs.org/sdr/IPXA2026100603252.md): Skin · dented · Sep 30, 2026 · N354UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL AT 5 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.3", 7" FROM T/E, AT 5 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL). BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS
- [SDR IPXA2026093002770](https://openairdocs.org/sdr/IPXA2026093002770.md): Trim Panel · detached · Sep 30, 2026 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > MAIN ENTRY DOOR SEAL TRIM CAME OFF WHEN CLOSING DOOR REINSTALLED SEAL ITEM 15 INTO RETAINER ITEM 20 PER IPC 52-11-02-10A NO AMM REFERENCE COULD BE FOUND FOR THE INSTALLATION OF THIS DOOR CUTOUT/LINING SEAL
- [SDR IPXA2026093001662](https://openairdocs.org/sdr/IPXA2026093001662.md): Seal · detached · Sep 30, 2026 · N329UP · Boeing 76734AF · Passenger/Crew Doors
  > FORWARD UPPER L1 DOOR SEAL PARTIALLY DETACHED. REINSTALLED FORWARD UPPER UNPRESSURIZED SEAL IN RETAINER OF FWD SIDE DOORWAY LINING PER AIPC 25-20-00-01B.
- [SDR IPXA2026093004390](https://openairdocs.org/sdr/IPXA2026093004390.md): Handle · binding · Sep 30, 2026 · N327UP · Boeing 76734AF · Life Raft
  > LIFE RAFT BIN HANDLE HARD TO OPEN LUBRICATED AS NEEDED. HANDLE. OPS CK OK
- [SDR IPXA2026100465120](https://openairdocs.org/sdr/IPXA2026100465120.md): Stiffener · cracked · Sep 28, 2026 · N354UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, STIFFENER CRACK AT CENTER FRONT BS 785.9 RBL 33. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV.96 AND EGAT WORK SHEET NO.60769 AND UPS SREO-58151-REQ001 REV2.
- [SDR IPXA2026100465056](https://openairdocs.org/sdr/IPXA2026100465056.md): Stiffener · cracked · Sep 28, 2026 · N354UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > STIFFENER CRACK AT CENTER FRONT BS 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2, REV 96 AND EGAT WORK SHEET NR 60770 AND SREO-58151-REQ001 REV 2.
- [SDR IPXA2026092829503](https://openairdocs.org/sdr/IPXA2026092829503.md): Handle · binding · Sep 25, 2026 · N312UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR CAPTURE LEVER STICKS IN INBOARD POSITION. ++ FOUND DOOE CREW ENTRY DOOR INTERLOCK PAWL WORN, REMOVED AND REPLACED INTERLOCK PAWL REF 767 M/M 52-11-26 OPERATED CREW ENTRY DOOR REF 767 M/M 52-12-00-862-001-001. DOOR OPERATES OK.
- [SDR IPXA2026092495235](https://openairdocs.org/sdr/IPXA2026092495235.md): Pawl · not seated · Sep 23, 2026 · N323UP · Boeing 76734AF · Passenger/Crew Doors
  > L FWD ENT DOOR SECURE HANDLE WILL NOT SEAT FOUND DEEP GOUGES IN ENTRY DOOR INTERLOCK PAWL. REPLACED INTERLOCK PAWL IAW AMM 52-11-26-404-003. OPS CHECK GOOD IAW AMM 52-11-26-710-801.
- [SDR IPXA2026092364703](https://openairdocs.org/sdr/IPXA2026092364703.md): Unknown · odor · Sep 22, 2026 · N324UP · Boeing 76734AF · Air Distribution System
  > VERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180 REF AMM 71-00-00-795-034-H03 TEST NO. 3 - GROUND TEST - IDLE LEAK TEST. RAN ENGINES FOR 15 MINUTES WITH NO NOXIOUS ODOR NOTED AT THIS TIME WHILE ENGINE 2 SOLE SOURCE OF BLE
- [SDR IPXA2026092379070](https://openairdocs.org/sdr/IPXA2026092379070.md): Accelerometer · oscillates · Sep 22, 2026 · N314UP · Boeing 76734AF · Flight Control System
  > DURING CLIMB EXPERIENCED NOTICABLE OSCILLATIONS COMING FROM THE TAIL THAT DISSIPATED AT CRUISE. ALL ENG INDICATIONS NORMAL VERTICAL STABILIZER ACCESS PANELS AND RH ELEVATOR PCU PANLES CLOSED IAW AMM 27-31-05 REV149. FOUND FAULT DURING YAW DAMPER SYSTEM BITE PR
- [SDR IPXA2026092264312](https://openairdocs.org/sdr/IPXA2026092264312.md): Warning Message · false activation · Sep 22, 2026 · N322UP · Boeing 76734AF · Leading Edge Slat Position Indicating System
  > EMERGENCY DECLARED ON APPROACH TO LANDING. FLAPS 25 SELECTED AND LE-SLAT DISAGREE EICAS CAME ON. TROUBLESHOT IAW FIM 27-51 FT 808, NO FAULTS NOTED. EXTENDED AND RETRACTED SLATS/FLAPS IAW AMM 27-81-00. OPS CHECKED GOOD.
- [SDR IPXA2026092264703](https://openairdocs.org/sdr/IPXA2026092264703.md): Unknown · odor · Sep 22, 2026 · N324UP · Boeing 76734AF · Air Distribution System
  > VERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180. PERFORMED GVI IN BOTH PACK BAYS WITH NO OBVIOUS FAULTS NOTED. DURING RIGHT ENGINE RUN, EXHAUST FUMES WERE DETECTED IN THE FLIGHT DECK. SWAPPING BETWEEN PACK 1 AND PACK 2
- [SDR IPXA2026092308451](https://openairdocs.org/sdr/IPXA2026092308451.md): Skin · ground damage · Sep 18, 2026 · N303UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, CAN BLEW OFF THE K LOADER DUE TO JET BLAST IS UNDER BELLY OF AIRCRAFT LT SIDE STATION 698-720 STRINGER S39-S36 FABRICATED FREEZE PLUG PER STEP 10 OF EO-98676-PRELIM2. SKIN REPAIR COMPLETED PER EO-98676-REQ1.
- [SDR IPXA2026092286713](https://openairdocs.org/sdr/IPXA2026092286713.md): Cowling · cracked · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED SKIN, NR 1 ENG RT CORE COWL LOWER FWD SKIN NEAR NO.1 LATCH. PERFORM REPAIR I.A.W UPS EO-98690-REQ1 REV.1.
- [SDR IPXA2026092191640](https://openairdocs.org/sdr/IPXA2026092191640.md): Panel · eroded · Sep 17, 2026 · N355UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > ERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.
- [SDR IPXA2026092289443](https://openairdocs.org/sdr/IPXA2026092289443.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED NR 1 NOSE COWL INLET AT 7 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026092290656](https://openairdocs.org/sdr/IPXA2026092290656.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED NR 1 ENG NOSE COWL INLET AT 5 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026092290813](https://openairdocs.org/sdr/IPXA2026092290813.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 TO 6:00 POS. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SAT
- [SDR IPXA2026092290842](https://openairdocs.org/sdr/IPXA2026092290842.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED NR 1 ENGINE NOSE COWL INLET AT 6 O'CLOCK POSITION. UT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( ‘ DIA: 0.2", 27" FROM FWD EDGE, 31.5" FROM UPPER EDGE ‘¡ DIA: 0.4", 32.4" FROM FWD EDGE, 31" FROM UPPER EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF
- [SDR IPXA2026092186627](https://openairdocs.org/sdr/IPXA2026092186627.md): Floor Panel · cracked · Sep 17, 2026 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > CRACKED PANEL, AFT CARGO FLOOR STRUCTURE, BS 1329, BL 0. REMOVED DAMAGE PANEL I.A.W SRM 51-40-02-0G REV. 96. INSTALLED FABRICATED PANEL I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 451T2612 SHEET 2 REV. B.
- [SDR IPXA2026091898870](https://openairdocs.org/sdr/IPXA2026091898870.md): Smoke Goggles · damaged · Sep 17, 2026 · N353UP · Boeing 76734AF · Emergency Equipment
  > CENTER SUPERNUMERARY SEAT SMOKE GOGGLES CRAZED AND BUBBLED REMOVED AND REPLACED CENTER SUPERNUMERARY SEAT SMOKE GOGGLES IAW MM 25-64-00
- [SDR IPXA2026092267592](https://openairdocs.org/sdr/IPXA2026092267592.md): Fairing · debonded · Sep 16, 2026 · N355UP · Boeing 76734AF · Aerodynamic Fairings
  > DEBONDED SKIN, RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES
- [SDR IPXA2026092166138](https://openairdocs.org/sdr/IPXA2026092166138.md): Skin · punctured · Sep 16, 2026 · N355UP · Boeing 76734AF · Landing Gear Doors
  > SKIN, RT MLG W/W DOOR MID PUNCTURED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1, 51-01-01, REV 144. REMOVE THE DELAMINATION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220
- [SDR IPXA2026092172110](https://openairdocs.org/sdr/IPXA2026092172110.md): Bracket · cracked · Sep 16, 2026 · N355UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026092172477](https://openairdocs.org/sdr/IPXA2026092172477.md): Angle · cracked · Sep 16, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT BULKHEAD REAR LT ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND DWG 313T2303 SH. 141 REV. A AND BOEING DWG NO. 313T2303 SH. 146 REV. -.
- [SDR IPXA2026092450293](https://openairdocs.org/sdr/IPXA2026092450293.md): Seal Depressor · corroded · Sep 15, 2026 · N316UP · Boeing 76734AF · Electrical/Electronic Compartment Doors
  > CORROSION - SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL FWD HINGE FWD SIDE BRACKET. REMOVED DAMAGE SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8610 SH.7 REV.D.
- [SDR IPXA2026092450484](https://openairdocs.org/sdr/IPXA2026092450484.md): Seal Depressor · corroded · Sep 15, 2026 · N316UP · Boeing 76734AF · Electrical/Electronic Compartment Doors
  > CORROSION - SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL AFT HINGE AFT SIDE BRACKET. REMOVED DAMAGE SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96. INSTALLED FABRICATED SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8610 SH.8 REV.D.
- [SDR IPXA2026092350550](https://openairdocs.org/sdr/IPXA2026092350550.md): Tee Angle · broken · Sep 15, 2026 · N316UP · Boeing 76734AF · Fuselage Main, Structure
  > - BROKEN - SPLICE TEE, LOWER FACE OF KEEL BEAM AT LOWER PANEL NO.149AL FWD SUPPORT, NEAR STA 962, LBL 5. REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8629 SH.2 REV.A.
- [SDR IPXA2026092347262](https://openairdocs.org/sdr/IPXA2026092347262.md): Angle · gouged · Sep 15, 2026 · N316UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR ON MAIN DECK FLOOR SUPPORT STRUCTURE, LOCATED AT APPROXIMATE STA. 710 OUTBD OF LT. FWD CARGO PIT SIDEWALL, IS GOUGED IN THREE PLACES. ACCOMPLISHED THE REPAIR I.A.W SRM 53-00-52-2R REPAIR 9 REV.96 AND EGAT WORK SHEET 60756.
- [SDR IPXA2026092350293](https://openairdocs.org/sdr/IPXA2026092350293.md): Seal Depressor · corroded · Sep 15, 2026 · N316UP · Boeing 76734AF · Accessory Compartment Doors
  > CORRODED SEAL DEPRESSOR, LOWER FUSELAGE LT ECS DOOR 193NL FWD HINGE FWD SIDE BRACKET.
- [SDR IPXA2026092350484](https://openairdocs.org/sdr/IPXA2026092350484.md): Seal Depressor · corroded · Sep 15, 2026 · N316UP · Boeing 76734AF · Accessory Compartment Doors
  > CORRODED SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL AFT HINGE AFT SIDE BRACKET.
- [SDR IPXA2026092150993](https://openairdocs.org/sdr/IPXA2026092150993.md): Former · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT BRACKET, NEAR WS 441.596. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:1142241 SH 4 REV: - AND UPS SREO-54290-REQ1 REV.3.

Next page: https://openairdocs.org/model/boeing-767-34af/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 = '76734AF'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-34af/reports

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