# Service difficulty reports: N77865

A list on [N77865](https://openairdocs.org/aircraft/N77865.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 3 · 114 reports

- [SDR CALA2026083118994](https://openairdocs.org/sdr/CALA2026083118994.md): Lamp · faulty · Aug 27, 2026 · N77865 · Boeing 75733N · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE, DOOR 2L EXTERIOR SLIDE LIGHT INOP. REPLACED THE LAMPS IAW AMM 33-51-06-962-001-002. OPS TESTED GOOD.
- [SDR CALA2026080918372](https://openairdocs.org/sdr/CALA2026080918372.md): Survival Kit · wrong part · Aug 5, 2026 · N77865 · Boeing 75733N · Emergency Equipment
  > VERIFY THE AIRCRAFT HAS THE CORRECT NUMBER OF SURVIVAL KIT PACK ASSY AND VERIFY SERIAL NUMBERS. INSPECTED AND FOUND 6 SURVIVAL KITS LOCATED ONBOARD IN 3 DROPDOWN OVERHEAD STORAGE BINS, 4 KITS LOCATED IN F/C CABIN, 2 KITS LOCATED IN THE VERY LAST OVHD BIN. S/N
- [SDR CALA2026031014475](https://openairdocs.org/sdr/CALA2026031014475.md): Charger · inoperative · Mar 9, 2026 · N77865 · Boeing 75733N · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - 1R EXIT IDENTIFIER SIGN INOP. R & R M731 EMERGENCY BATTERY CHARGER, IAW AMM 33-51-07-862-029-002. OPS CHECK GOOD.
- [SDR CALA2026011913049](https://openairdocs.org/sdr/CALA2026011913049.md): Skin · corroded · Jan 14, 2026 · N77865 · Boeing 75733N · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN INTERNAL BETWEEN BS 879 - 900 BLIGE CENTER LINE HAS CORROSION (EXFOLIATED). REPAIR ACCOMPLISHED IAW ECRA 5330-07683. MAJOR REPAIR. PERFORMED A REPAIR IAW VT MAE 757-5330-13-A4231, ATTACHED TO EC/RA AS FIGURE 1 THROUGH 35 WITH NO DEVIATIONS IAW
- [SDR CALA2026012813411](https://openairdocs.org/sdr/CALA2026012813411.md): Frame · dented · Jan 11, 2026 · N77865 · Boeing 75733N · Fuselage Main, Plate/Skin
  > DURING C-CHECK, MX REPORTED ONE DENT ON INBD FLANGE OF BS 500 FRAME, S-15L & 16L. ACCOMP A REPAIR IAW ECRA 5330-07671, PART 1, STEP 1 WITH NO DEVIATIONS.
- [SDR CALA2026012713358](https://openairdocs.org/sdr/CALA2026012713358.md): Skin · corroded · Jan 11, 2026 · N77865 · Boeing 75733N · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THREE CORROSION DAMAGES ON BS 1420 FRAME BOTTOM BETWEEN S29L & S30, S29R & S30 AND S28R & S29R. PERFORMED A REPAIR IAW 757-5360-13-A4238,
- [SDR CALA2026012813413](https://openairdocs.org/sdr/CALA2026012813413.md): Frame · corroded · Jan 9, 2026 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > DURING C-CHECK, THREE CORROSION DAMAGES ON BS 1420 FRAME BTWN S29-30L, S29-30R & S28-29R. MAJOR REPAIR ACCOMPLISHED AND ALL RII STEPS C/W.
- [SDR CALA2026012813412](https://openairdocs.org/sdr/CALA2026012813412.md): Frame · corroded · Jan 9, 2026 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > CORROSION DAMAGE ON BS 1460 FRAME BOTTOM BETWEEN S29 -30R. PERFORMED AN INSPECTION IAW PART 2 OF THE LATEST REVISION OF ECRA 5360-02086. ACCOMPLISHED MAJOR REPAIR AND ALL RII STEPS C/W. DIP APPROVED FOR INSPECTION OF DAMAGE.
- [SDR CALA2026010712745](https://openairdocs.org/sdr/CALA2026010712745.md): Frame · dented · Jan 4, 2026 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > BULK CARGO, BS 1480, LOWER SIDEWALL, S26 - 27L, FRAME HAD A DENT. ACCOMPLSHED REPAIR IAW EA 757-5360-13-A4239, FIGURE 1 - 7, WITH NO DEVIATIONS IAW EC/RA 5360-02081 ACCOMPLISHED MAJOR REPAIR AND C/W ALL RII STEPS IAW GMM 09-25-05.
- [SDR CALA2026012813414](https://openairdocs.org/sdr/CALA2026012813414.md): Frame · dented · Jan 2, 2026 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > DURING C-CHECK, MAINTENANCE REPORTED ONE DENT, BS 1480 FRAME BOTTOM BTWN S26-27L. THE DENT MEASURED 0.860 INCH LONG, 0.390 INCH WIDE, AND 0.011 INCH DEEP. ACCOMPLISHED A REPAIR IAW ECRA 5360-02081, PART 1, STEP 1WITH NO DEVIATIONS.
- [SDR CALA2026012713356](https://openairdocs.org/sdr/CALA2026012713356.md): Frame · dented · Jan 2, 2026 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > DURING C-CHECK, MAINTENANCE REPORTED ONE DENT ON BS 1480 FRAME BOTTOM BETWEEN S26L AND S27L. THE DENT MEASURED 0.860 INCH LONG, 0.390 INCH WIDE, AND 0.011 INCH DEEP.
- [SDR CALA2026012713355](https://openairdocs.org/sdr/CALA2026012713355.md): Frame · dented · Jan 2, 2026 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > DURING THE C-CHECK MAINTENANCE REPORTED ONE DENT ON INBD FLANGE OF THE BS 500 LT FRAME BTWN S15L AND S16L. MAJOR REPAIR
- [SDR CALA2026011212865](https://openairdocs.org/sdr/CALA2026011212865.md): Frame · corroded · Dec 24, 2025 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > AFT CARGO, FLOOR AREA, BS 1460, BTWN STG 29R TO STG 30, FRAME HAS CORROSION. PART FABRICATED IN HOUSE PER DWG146N2063 AND DWG 140N2063. PERFORMED A REPAIR IAW 757-5360-13-A4229 1 THROUGH 9 WITH NO DEVIATIONS EC/RA:5360-02086.
- [SDR CALA2026011212864](https://openairdocs.org/sdr/CALA2026011212864.md): Frame · corroded · Dec 24, 2025 · N77865 · Boeing 75733N · Fuselage Main, Frame
  > AFT CARGO, FLOOR AREA, BS 1420, BTWN S29L - 28R, FRAME HAS CORROSION. PART FABRICATED IAW DWG 146N5426, REV A. PERFORMED A REPAIR IAW 757-5360-13-A4238 F IGURES 1 THROUGH 12 WITH NO DEVIATIONS EC/RA:5360-02087.
- [SDR CALA2025123012522](https://openairdocs.org/sdr/CALA2025123012522.md): Floor Support · corroded · Dec 24, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > AFT CARGO, FLOOR SUPPORT, BS 1400 - 1420, S29 - 30L., CORRODED. REMOVED IAW SRM 53-60-04-1A-0, FIG 101, SHEET 2, DETA IL II. FABRICATED A NEW FLOOR SUPPORT AND BRACKET, AND INSTALLED IAW SRM 51-40-02.
- [SDR CALA2025123012521](https://openairdocs.org/sdr/CALA2025123012521.md): Floor Support · corroded · Dec 24, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > AFT CARGO, FLOOR SUPPORT, BS 1400 - 1420, S29 - 30R, CORRODED. BLENDED REPAIR WITHIN LIMITS.
- [SDR CALA2025122312377](https://openairdocs.org/sdr/CALA2025122312377.md): Window Frame · dented · Dec 20, 2025 · N77865 · Boeing 75733N · Fuselage Main, Structure
  > MAIN CABIN, LT BS 500 BELOW PASSENGER WINDOW FRAME HAD A DENT. REPAIRED THE WINDOW FRAME BS 500 BTW S15L AND S16L IAW EC/RA 53 30-07671 AND EA 757-5330-13-A4230, REV-. MAJOR REPAIR ACCOMPLISHED AND ALL RII STEPS VERIFIED.
- [SDR CALA2025122312361](https://openairdocs.org/sdr/CALA2025122312361.md): Bracket · corroded · Dec 20, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > BULK CARGO, BS 1520 ABOVE STRINGER 30R, ANGLE BRACKET WAS CORRODED. R & R THE BRACKET BS 1520, S20 - 30R IAW SRM 51-40-02-OG-0.
- [SDR CALA2026010212591](https://openairdocs.org/sdr/CALA2026010212591.md): Floor Support · corroded · Dec 19, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > BULK CARGO, BETWEEN BS 1500 - 1520, FLOOR SUPPORTS HAVE CORROSION AT NUTPLATES AREA (4 PLACES). PART FABRICATED REMOVED AND REPLACED FLOOR SUPPORT AT AFT CARGO COMP BS 1500 TO 1520 IAW SRM 51-40-02-0G-0.
- [SDR CALA2025122312346](https://openairdocs.org/sdr/CALA2025122312346.md): Floor Support · corroded · Dec 19, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > BULK CARGO, FLOOR AREA, CLOSE TO BS 1500, BETWEEN S29 - 30, FLOOR SUPPORT SPLICE HAS CORROSION. REMOVED AND REPLACED TWO FLOOR SUPPORT SPLICES IN THE AFT CARGO BAY. BETWEEN BS 1500 - 1520 IAW SRM 51-40-02-0G-0.
- [SDR CALA2025122312344](https://openairdocs.org/sdr/CALA2025122312344.md): Drag Fitting · cracked · Dec 19, 2025 · N77865 · Boeing 75733N · Nacelle/Pylon, Attach Fittings
  > NDT ROTO INSPECTION ON NR 1 ENG PYLON DRAG FITTING. NOTED A CRACK IN HOLE NR 8 AT TOP OF SKIN AT THE 3 O'CLOCK. ACCOMPLISHED A REPAIR IAW EA 757-5720-13-A4226, AND EC/RA 57 20-03596, PART 1 STEP 1.
- [SDR CALA2025121912257](https://openairdocs.org/sdr/CALA2025121912257.md): Longeron · corroded · Dec 17, 2025 · N77865 · Boeing 75733N · APU Cowling/Containment
  > APU COMPARTMENT LT BS 1885-1890 ABOVE APU DOOR LONGERON, METALIC HONEYCOMB SKIN INNER SURFACE CORRODED. REPAIRED AREA OF APU COMPT. LT BS 1885-1890 IAW SRM 51 -70-10-2R-0. PERFORMED POST CURE INSPECTION IAW NTM PART 451-00-03. DISBOND - DELAMINATION FREE.
- [SDR CALA2025121912255](https://openairdocs.org/sdr/CALA2025121912255.md): Skin · cracked · Dec 17, 2025 · N77865 · Boeing 75733N · Passenger/Crew Doors
  > EA 5210-03219 REV C: L4 ENTRY DOOR INTERNAL STRUCTURE CRACKED WITH LOCAL PERFORATION THROUGH SKIN, LOCATED BTWN THE UPPER HINGE FITTING AREA. PERFORMED REPAIR IAW EA 757-5210-13-A4216, ATTACHED TO THIS ECRA AS FIGURES 1 THROUGH 15 WITH NO DEVIATION S ALLOWED.
- [SDR CALA2025122212292](https://openairdocs.org/sdr/CALA2025122212292.md): Fitting · cracked · Dec 13, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > L2 DOOR CUTOUT, FWD FRAME, MECHANISM, SUPPORT STRUCTURE IS CRACKED. REMOVED AND REPLACED FITTING ON L2 DOOR FWD CUTOUT FRAME BS 684 -692.38. IAW SRM 51-40-02-0G, DWG 143N8375.
- [SDR CALA2025122412387](https://openairdocs.org/sdr/CALA2025122412387.md): Angle · corroded · Dec 12, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > FUSELAGE APU INLET DOOR CUTOUT BS 1825, STRINGERS 3-6R, INNER STRAP HAS EXFOLIATION. AFT STRAP WAS REPAIRED IAW SRM 53-80-15-2R-1, REPAIR 1, FIGURE 202, DETAIL I AND TWO ANGLES SUPPORT AND ONE FWD STRAP WERE REMOVED AND REPLACED IAW SRM 51-40-02-0G-0. COMPL
- [SDR CALA2025121512096](https://openairdocs.org/sdr/CALA2025121512096.md): Plug · damaged · Dec 12, 2025 · N77865 · Boeing 75733N · Engine (Turbine/Turboprop)
  > (SDR)(19-0671-1-0004) CUSTOMER REQUEST - DO A HIDDEN DAMAGE INSP ECTION AT NUMBER 2 ENG DUE TO A BORESCOPE PLUG MISSING AT THE LP COMPRESSOR I/B UPR FAIRING AREA. REF NRC 138155. SDR WAS ENTERED. ACCOMPLISHED E2 LP COMPRESSOR FAIRING AREA HIDDEN DAMAGE INSPECT
- [SDR CALA2025121512094](https://openairdocs.org/sdr/CALA2025121512094.md): Plate · corroded · Dec 12, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF TRANSITION PANEL AFT CARGO COMPARTMENT FR1380/S26R-S27R, FOUND PLATE WITH CORROSION. REF N RC 137865. REMOVED AND REPLACED SPLICE AT AFT CARGO COMP. BETWEEN STA 1380 TO STA 1440 RH SIDE IAW B757-300 SRM 51-40-02-0G-0. REF NRC 1378 65.
- [SDR CALA2026011913084](https://openairdocs.org/sdr/CALA2026011913084.md): Transition Panel · corroded · Dec 8, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > BULK CARGO, FLOOR AREA, BS 1520, RT TRANSITION PANEL LOWER SURFACE HAS CORROSION. PERFORMED REPAIR AT TRANSITION PANEL BS 1520 TO 1640 IAW SRM 53-00-53-2R-2.
- [SDR CALA2025121011990](https://openairdocs.org/sdr/CALA2025121011990.md): Stringer Clip · corroded · Dec 8, 2025 · N77865 · Boeing 75733N · Fuselage Main, Attach Fittings
  > STRINGER CLIP CORRODED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-OG-0.
- [SDR CALA2025121011988](https://openairdocs.org/sdr/CALA2025121011988.md): Skin · corroded · Dec 8, 2025 · N77865 · Boeing 75733N · Fuselage Main, Structure
  > AFT CABIN METALIC PRESSURE DECK BETWEEN BS 1680 - 1720, UPPER SURFACE CORRODED BETWEEN LT CREASE BEAM TO RT CREASE BEAM. REF NRC 137952. REMOVED CORROSION AT AFT CABIN FLOOR METALIC PRESSURE DECK BETWE EN BS 1680 - 1720 UPPER SURFACE AND FOUND WITHIN LIMITS
- [SDR CALA2025120811873](https://openairdocs.org/sdr/CALA2025120811873.md): Angle · corroded · Dec 5, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF TRANSITION PANEL AT AFT CARGO BAY BS 1360 - 1380, S26R - S27R, FOUND WEB ASSY WITH CORROSION. REMOVED AND EVALUATED DAMAGE AT WEB ASSY AND FOUND WITHIN LIMITS IAW SRM 53-60-04-1A, AFTER FURTHER EVALUATION CORROSION IN ANGLE NOTED, EVALUATE
- [SDR CALA2025120811867](https://openairdocs.org/sdr/CALA2025120811867.md): Tee Angle · corroded · Dec 5, 2025 · N77865 · Boeing 75733N · Fuselage Main, Attach Fittings
  > CORROSION FOUND AT TEE CHORD LOWER SURFACE AT BS 900 BOTTOM SECTION. PERFORMED TEE CHORD REPAIR ON BS 900 BOTTOM, FABRICATED PARTS ON TRAVELER'S T25/1841651, T25/1841652 AND T25/1841653 IAW SRM 51-70-06, APPLIED TREAT, PRIMER, TOP COAT AND CIC.
- [SDR CALA2025120511807](https://openairdocs.org/sdr/CALA2025120511807.md): Bracket · cracked · Dec 4, 2025 · N77865 · Boeing 75733N · Aerodynamic Fairings
  > ONE BRACKET CRACKED AT THE LOWER LEFT WING OT BODY FAIRING STRUCTURE AT BS 1040, LOCATED AT THE FWD END OF THE BEAM. REMOVED AND REPLACED THE BRACKET ON LT WTB FAIRING STRUCTURE AT BS 1040 IAW SRM 51-40-02-0G. & DWG 149N7553.
- [SDR CALA2025120811847](https://openairdocs.org/sdr/CALA2025120811847.md): Bracket · corroded · Dec 3, 2025 · N77865 · Boeing 75733N · Fuselage Main, Plate/Skin
  > RIGHT UPPER WTB, UNDER FAIRINGS, BTWN BS 1080 - 1100, PANEL BRACKET SUPPORT HAS CORROSION. REMOVED AND REPLACED TEE BRACKET ON RT WING UPPER WTB STRUCTURE AT BS 1080 IAW SRM 51-40-02-0G, DWG 149N7552.
- [SDR CALA2025120411773](https://openairdocs.org/sdr/CALA2025120411773.md): Channel · corroded · Dec 3, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > L1 DOOR LOWER CUTOUT ATTACHED INTERCOSTAL CORRODED. REMOVED AND REPLACED TWO EA CHANNELS AT L1 DOOR LOWER CUTOUT IAW SRM 51-40-02-0G-0.
- [SDR CALA2025120211640](https://openairdocs.org/sdr/CALA2025120211640.md): Crease Beam · corroded · Nov 28, 2025 · N77865 · Boeing 75733N · Fuselage Main, Structure
  > (SDR) MAIN DECK RH SIDE CREASE BEAM BETWEEN STA 1290 AND STA 140 0 HAS CORROSION EXFOLIATED. ESFR ENTRY CREASE BEAM WAS EXFOLIATED REMOVE DAMAGE CREASE BEAM IAW SRM 51- 40-02, FABRICATED NEW CREASE BEAM, TRAVELER:T25/1841659, LOCATED AND DRILLED IAW SRM 51-40-
- [SDR CALA2025112711524](https://openairdocs.org/sdr/CALA2025112711524.md): Floor Support · corroded · Nov 26, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR AREA RBL 1 AT FR 352 FLOOR SUPPORT HAS SURFACE CORROSION. PERFORMED REPAIR AT MAIN DECK FLOOR SUPPORT BETWEEN RBL 1 FR 352 IAW SRM 51-70-11-0G-0.
- [SDR CALA2025112111396](https://openairdocs.org/sdr/CALA2025112111396.md): Seat Track · corroded · Nov 20, 2025 · N77865 · Boeing 75733N · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CABIN SEAT TRACK CENTER OF CROWN, LBL 46, BS 1080 - 1180. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02-0G-0.
- [SDR CALA2025112111394](https://openairdocs.org/sdr/CALA2025112111394.md): Seat Track · corroded · Nov 20, 2025 · N77865 · Boeing 75733N · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CABIN SEAT TRACK CENTER OF CROWN RBL 46, BS 1060 - 1180. REMOVED CORROSION IAW AMM 51-00-53-102-054; EVALUATED AS FOLLOW 0. THICKNESS 0.185", MATERIAL LOSS 0.050", MATERIAL REMAINING 0.135", FOUND TO BE WITHIN LIMITS IAW SRM 53-00-5 2-1A-1, FABRI
- [SDR CALA2025111911336](https://openairdocs.org/sdr/CALA2025111911336.md): Floor Support · corroded · Nov 17, 2025 · N77865 · Boeing 75733N · Fuselage Miscellaneous Structure
  > CORROSION UNDER THE NUTPLATE AT CABIN FLOOR STRUCTURE BS 353 RBL 24. REMOVED CORROSION AT CABIN FLOOR STRUCTURE STA 353 RBL 24 IAW B7 57-300 SRM 51-10-02-0G, CHECKED LIMITS MATERIAL LOSS 0.016" MAX ALLOWED IS 0.006 OF THICKNESS ORIGINAL 0.063" FOUND TO BE OUT
- [SDR CALA2025111911334](https://openairdocs.org/sdr/CALA2025111911334.md): Frame · corroded · Nov 17, 2025 · N77865 · Boeing 75733N · Fuselage Main, Structure
  > AFT CARGO, FLOOR AREA, BS 1440, BTWN S29 - 30L, FRAME HAS CORROSION. REMOVED AND REPLACED DOUBLER IAW SRM 53-60-07-1A-0, SRM 51-40- 02, & DWG 146N1013, REV B. RESTORED SURFACE PROTECTION IAW SRM 51-20-01 & AMM 51-21-15.
- [SDR CALA2025091108792](https://openairdocs.org/sdr/CALA2025091108792.md): Valve · malfunctioned · Sep 7, 2025 · N77865 · Boeing 75733N · Pneumatic System
  > LEFT ENG HIGH STAGE EICAS C, THE LEFT ENGINE HPSOV IS CLOSED BECAUSE THE HIGH STAGE BLEED PRESSURETOO HIGH. CREW ABORTED TAKEOFF AT APPROX 20KTS. REF MEL 3611P FOR HPSOV DDP ACCOMPLISHED REQUEST MEL ON #1 ENG. MEL HAS BEEN COMPLIED WITH AND VALVE LOCKED OUT
- [SDR CALA2025081807861](https://openairdocs.org/sdr/CALA2025081807861.md): Oil System · overserviced · Aug 15, 2025 · N77865 · Boeing 75733N · APU Oil System
  > FAULT LIGHT ON DURING APU START. SECOND ATTEMPT MADE AFTER CLEARING FAULT. PERFORMED APU ECB BITE IAW FIM 49-11 TASK 875 & NOTED LOW OIL PRESSURE FLAG ON LAST 3 RUNS. REJECTED HMG MUST WORK DISREGARD PREVIOUS CALL, CONFIG ISSUE, HMG CURRENTLY FUNCTIONAL OPS
- [SDR CALA2025081107567](https://openairdocs.org/sdr/CALA2025081107567.md): Skin · gouged · Aug 9, 2025 · N77865 · Boeing 75733N · Fuselage Main, Plate/Skin
  > IMPACT DAMAGE TO SKIN WITH MULTIPLE DEEP SCRATCHES & GOUGES, JUST BELOW & AFT OF AFT CARGO DOOR, BETWEEN S27R & 28R RUNNING FROM APPROX 6" FWD OF FRAME 1460 TO APPROX 10" AFT OF FRAME 1500.AFTER INITIAL EVALUATION DAMAGE IS 55 INCHES LONG. SOME OF THE GOUGES
- [SDR CALA2025080707410](https://openairdocs.org/sdr/CALA2025080707410.md): Bottle · no discrepancy · Aug 4, 2025 · N77865 · Boeing 75733N · Standard Practices/Structures
  > R2 DOOR SLIDE AND BOTTLE, PLEASE VERIFY R2 DOOR-MOUNTED ESCAPE SLIDE BOTTLES EXPIRATION DATE AND THE SLIDE EXPIRATION DATE AND CONTACT TOMC WITH THE DATES ON BOTH AND DOCUMENT HERE ALSO PLEASE RECORD THE SLIDE P/N AND SN AND THE BOTTLE P/N AND S/N ON THIS LOG
- [SDR CALA2025072206840](https://openairdocs.org/sdr/CALA2025072206840.md): Access Door · missing · Jul 18, 2025 · N77865 · Boeing 75733N · Nacelle/Pylon, Main Frame
  > PDA 1 ENG #2 OIL SERVICING DOOR MISSING ON ARRIVAL. PRESUME PANEL DEPARTED FROM AC LOGPAGES 5605104, 5605196 ASSOCIATED WITH THIS LOGPAGE... INSTALLED NEW OIL SERVICING DOOR ON ENG #2 REF AMM 71-11-04-038-075-R00.
- [SDR CALA2025063006044](https://openairdocs.org/sdr/CALA2025063006044.md): Handle · false indication · Jun 26, 2025 · N77865 · Boeing 75733N · Door Warning System
  > DOOR 2L SLIDE LIGHT NOT ILLUMINATING WITH HANDLE ARMED. CYCLED DOOR HANDLE AND CHEKED OK. NO MX ACTION. OPS CHECKS GOOD MULTIPLE TIMES.
- [SDR CALA2025062605931](https://openairdocs.org/sdr/CALA2025062605931.md): Idg · faulty · Jun 22, 2025 · N77865 · Boeing 75733N · AC Generator-Alternator
  > GENERATOR DRIVE SYSTEM EICAS MESSAGE (01=L,02=R) GEN DRIVE DISPL AYED. GEN DRIVE LIGHT ON. GEN DRIVE DISCONNECTED 02 ON CLIMB OUT COMPLETED CHECKLIST"R IDG OIL LEVEL" MSG PERFORMED BPCU BITE IN REFERENCE TO 24-20 FAULT TREE 801 AND FOUND THE FOLLOWING MESSAGES
- [SDR CALA2025040103390](https://openairdocs.org/sdr/CALA2025040103390.md): Battery Pack · inoperative · Mar 28, 2025 · N77865 · Boeing 75733N · Emergency Lighting
  > (SUPPORT TASK) EMERGENCY PACK AT LOCATION M11486 THAT FAILED OPS CHECK AND WAS REEMOVED AND REPLACED ON LOG PAGE 9286036, BATTERY PACK WAS REMOVED AND REPLACED IAW B757 AMM 33-51-07 ON LOGPAGE 9286036.
- [SDR CALA2025040103389](https://openairdocs.org/sdr/CALA2025040103389.md): Battery Pack · inoperative · Mar 28, 2025 · N77865 · Boeing 75733N · Emergency Lighting
  > (SUPPORT TASK) EMERGENCY BATTERY PACK AT LOCATION M736 THAT FAILED OPS CHECK AND WAS REMOVED AND REPLACED ON LOG PAGE 9286036. BATTERY PACK WAS REMOVED AND REPLACED IAW B757 AMM 33-51-07 ON LOG PAGE 9286036,

Next page: https://openairdocs.org/aircraft/N77865/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 = 'N77865' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N77865/reports

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