N7834A
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
69 reports on file, 2015-06-18 – 2020-06-21.
Part: SKIN — GOUGED (BS 500) · airframe 50,580 hrs · 26,571 cycles
GOUGE FOUND IN THE SKIN AT STRINGER 19L + 5.5' AT BS 500, GOUGE APPROXIMATELY 9.25 LONG. REPAIRED IAW SRM 53-00-01-2R-36 REPAIR 36. CATEGORY B REPAIR.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,039 hrs · 26,228 cycles
ONE EMERGENCY LIGHTS BATTERY PACK FAILED A CAPACITY TEST. REMOVED & REPLACED THE BATTERY PACK IAW AMM 33-51-06, AND DWG 33500005.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,039 hrs · 26,228 cycles
RIGHT LOWER HORIZONTAL STABILIZER SKIN HAD A L=.750" CRACK LOCATED 16 5/8 INCHES AFT OF FRONT SPAR AT STAB LE STA 199.23. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11, REPAIR 11. THIS IS A CATEGORY B REPAIR. PERFORM A DVI AND AN EXTERNAL LOW FREQUENCY EDDY CURRENT (LFEC) INSPECTION OF THE EXTERNAL PART 1 DOUBLER AND INSPECT THE SKIN UNDER THE EXTERNAL PART 1 DOUBLER AT 56000 TOTAL FLIGHT.
Part: PANEL — BROKEN (KEELBEAM) · airframe 50,039 hrs · 26,228 cycles
LOWER FWD KEEL BEAM PANEL 192E FWD INBD AND OUTBD ATTACH BRACKETS BROKEN. / REMOVED AND REPLACED LOWER FWD KEEL BEAM PANEL 192E FWD INBD AND OUTBD ATTACH BRACKETS PER SRM 51-40-02.
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 50,039 hrs · 26,228 cycles
RH STABILIZER UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED RH STABILIZER UPPER SLIDING SEAL PER AMM.53-31-31
Earlier reports · 2015–2019 · 64 reports
2019
Part: CONNECTOR — LOOSE (CABIN) · airframe 48,802 hrs · 25,469 cycles
EMERGENCY EXIT LIGHTS INOP. CONNECTED CONNECTORS IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,802 hrs · 25,469 cycles
EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — UNSECURE (CABIN) · airframe 48,802 hrs · 25,469 cycles
EXTERIOR EMERGENCY LIGHT INOP. SECURED BATTERY PACK TO EMERGENCY LIGHT POWER SUPPLY PER AMM.
Part: CONNECTOR — LOOSE (EXIT SIGN) · airframe 48,802 hrs · 25,469 cycles
EXIT SIGN EMERGENCY LIGHT INOP. RECONNECTED CONNECTOR PER AMM.
Part: LENS — MISSING (EXIT SIGN) · airframe 48,802 hrs · 25,469 cycles
EXIT SIGN MISSING LENS. REPLACED LENS IAW AMM.
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 48,802 hrs · 25,469 cycles
LT VAPOR BARRIER CRACKED LBL 26 WL 150, BETWEEN FASTENER HOLE UNDER VERTICAL STIFFENER AND EDGE. REPAIRED VAPOR BARRIER IAW SRM.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,802 hrs · 25,469 cycles
RIGHT HORIZONTAL STABILIZER HAD A CRACKED STIFFENER ON RIB NR 5 AT STAB STA. 129.5, THIRD STIFFENER AFT OF LEADING EDGE. REPAIRED STIFFENER IAW SRM.
Part: ANGLE — CORRODED (BS 312-328) · airframe 48,802 hrs · 25,469 cycles
R1 LOWER MAIN SILL WEB ANGLE CORRODED AROUND FASTENER HOLES BETWEEN BS. 312 TO BS. 328, RBL 50. / R&R WEB ANGLE IAW SRM AND DWG.
Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 48,802 hrs · 25,469 cycles
FORWARD MAIN CABIN FLOOR PANEL 221BF HAD CORRODED INSERT, BETWEEN BS. 270 TO BS. 420. R&R FLOOR PANEL 221BF CORRODED INSERT IAW SRM & DWG.
Part: TIE DOWN — CORRODED (L1 DOOR SLIDE) · airframe 48,802 hrs · 25,469 cycles
L1 ESCAPE SLIDE TIE DOWN CORRODED AT BS. 344.65, LBL 57.45. R&R TIE DOWN IAW AMM AND DWG.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 48,802 hrs · 25,469 cycles
INTERCOSTAL CRACKED AT FASTENER HOLE BETWEEN BS. 312 TO BS. 328, LBL 47. / R&R INTERCOSTAL IAW SRM AND DWG.
Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 48,802 hrs · 25,469 cycles
FORWARD MAIN CABIN FLOOR PANEL 221DF HAD CORRODED INSERT, BETWEEN BS. 270 TO BS. 420. / R&R FLOOR PANEL 221DF IAW SRM & DWG.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 48,802 hrs · 25,469 cycles
AFT CARGO DOOR THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847, RBL 27. R&R WEB IAW SRM & DWG.
Part: ANGLE — CRACKED (BS 480 BAFFLE) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO BAFFLE CLIP CRACKED AT BS. 480, LBL 24. R&R BAFFLE CLIP PER SRM AND DWG.
Part: CHANNEL — CORRODED (BS 500D) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO L/H ZEE-CHANNEL CORRODED AT BS. 500D, LBL 24. R&R ZEE CHANNEL IAW SRM & DWG.
Part: ANGLE — CRACKED (BS 500C) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO BAFFLE CLIP CRACKED AT BS. 500C, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.
Part: GUSSET — CRACKED (BS 500D) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM & DWG.
Part: SHIELD — CORRODED (BS 492-500A) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO AFT SHIELD CORRODED BETWEEN BS. 492 TO BS. 500A, RBL 24. R&R SHIELD IAW SRM AND DWG.
Part: GUSSET — CRACKED (BS 500D) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM & DWG.
Part: ANGLE — CORRODED (BS 500A-500D) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO R/H AFT ZEE-CHANNEL CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 24. / R&R SIDE PLATE ANGLE IAW SRM AND DWG.
Part: ANGLE — CRACKED (BS 500B) · airframe 48,802 hrs · 25,469 cycles
FORWARD CARGO BAFFLE CLIP CRACKED AT BS. 500B, LBL 24. / R&R BAFFLE CLIP PER SRM AND DWG.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 48,802 hrs · 25,469 cycles
RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 48,802 hrs · 25,469 cycles
LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS. 663, LBL 34. REPAIRED WEB IAW SRM.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 48,802 hrs · 25,469 cycles
EXTERNAL POWER DOOR CUTOUT CRACKED IN 2 PLACES ON AFT EDGE. REPAIRED DOUBLER IAW SRM.
Part: RIVET — LOOSE (R1 GIRT BAR) · airframe 48,174 hrs · 25,038 cycles
R1 DOOR SLIDE GIRT BAR CLIP LOOSE. R&R RIVET PER SRM.
Part: ISOLATOR — BROKEN (R1 DOOR) · airframe 48,174 hrs · 25,038 cycles
R1 DOOR SLIDE PACK MOUNTING BRACKET ISOLATOR BROKEN. R&R ISOLATOR PER SRM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,167 hrs · 24,381 cycles
L1 DOOR GIRT BAR DOOR LOOSE. REPOSITIONED SLIDE PER MT.
2018
Part: PROXIMITY SENSOR — FAULTY (LE SLAT) · airframe 45,626 hrs · 23,376 cycles
DECLARED EMERGENCY, LEADING EDGE FLAPS TRANSIT LIGHT ON DURING CONFIGURING FOR LANDING RAN APPROPRIATE CHECKLIST & LANDED FLAPS / 15. R&R NR 7 SLAT INBOARD PROXIMITY SENSOR PER AMM.
Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 43,831 hrs · 22,232 cycles
LT WING FORWARD WING TO BODY 197AL AFT SUPPORT ANGLE FRAME CRACKED. R&R ANGLE PER SRM.
2017
Part: MOUNT — LOOSE (L1 DOOR) · airframe 42,468 hrs · 21,326 cycles
L1 DOOR EMERGENCY EVAC SLIDE MOUNT ATTACHMENTS LOOSE. R&R MOUNT ASSEMBLY IAW AMM.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 42,244 hrs · 21,173 cycles
AFT CARGO THRESHOLD WEB CRACKED AT 31.75' FROM FORWARD EDGE AND 1.5" FROM OUTBOARD EDGE. REPAIRED WEB PER SRM.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 42,046 hrs · 21,037 cycles
R1 DOOR LOWER EMERGENCY LIGHT LENS CRACKED. R & R THE LENS IAW AMM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,493 hrs · 20,709 cycles
R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW MM.
2016
Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 39,784 hrs · 19,667 cycles
L2 DOOR EMERGENCY EVAC SLIDE GIRT LOOSE. SECURED GIRT PER MT.
Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 39,784 hrs · 19,667 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT LOOSE. SECURED GIRT PER MT.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,473 hrs · 18,881 cycles
R1 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED THE LAMP IN THE SIGN IAW AMM.
2015
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 35,444 hrs · 17,165 cycles
FORWARD RT SERVICE DOOR EMER LIGHT ON HEADER PANEL INOPERATIVE. R & R FWD CONNECTOR IAW AMM.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 35,443 hrs · 17,165 cycles
R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.
Part: LIGHT — DISCONNECTED (EXIT SIGN) · airframe 35,444 hrs · 17,165 cycles
RIGHT OVERWING EMER EXIT SIDEWALL SIGN, LIGHT INOPERATIVE AFT OF EXIT. FOUND LIGHT DISCONNECTED. CONNECTED SIGN IAW AMM.
Part: LIGHT — DISCONNECTED (CABIN) · airframe 35,444 hrs · 17,165 cycles
L1 DOOR EMER EXIT LIGHT INOPERATIVE. FOUND LIGHT DISCONNECTED. CONNECTED LIGHT IAW AMM.
Part: LIGHT — DISCONNECTED (CABIN) · airframe 35,444 hrs · 17,165 cycles
R1 DOOR EMER EXIT LIGHT INOPERATIVE. FOUND LIGHT DISCONNECTED. CONNECTED LIGHT IAW AMM.
Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
R1 DOOR CUT OUT, UPPER HINGE SUPPORT FITTING FOR TORQUE TUBE CRACKED. R & R FITTING IAW SRM & DWG.
Part: HOUSING — BROKEN (CABIN) · airframe 35,444 hrs · 17,165 cycles
AFT ENTRY CEILING EMER EXIT LIGHT MOUNTING SCREWS INSERTS BROKEN. R & R LIGHT HOUSING IAW SRM.
Part: SHIM — BROKEN (LT WING) · airframe 35,444 hrs · 17,165 cycles
LEFT CTR WING TANK RIB 2 INBD SIDE SHIM BROKEN. R & R SHIM IAW DWG.
Part: SHIM — BROKEN (RT WING) · airframe 35,444 hrs · 17,165 cycles
RIGHT CTR WING TANK RIB 2 INBD SIDE SHIM BROKEN. R & R SHIM IAW DWG.
Part: SHIM — BROKEN (LT WING) · airframe 35,444 hrs · 17,165 cycles
LEFT CTR WING TANK RIB 2 OTBD SIDE SHIM BROKEN. R & R SHIM IAW DWG.
Part: SKIN — CRACKED (LE SLAT) · airframe 35,444 hrs · 17,165 cycles
RIGHT WING NR 5 LE SLAT NOSE SKIN CRACKED. REPAIRED NR 5 SLAT IAW SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 35,444 hrs · 17,165 cycles
LEFT WING NR 1 LE SLAT LOWER NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FORWARD GALLEY DOOR SURROUND LOWER STUB FRAME ANGLE CRACKED AT BS 296, RBL 60. REPAIRED ANGLE IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FORWARD SEAT TRACK FASTENER HOLES CRACKED AT BS 727B, LBL 45.5, OUTBOARD FORWARD, OUTBOARD AFT, INBOARD FORWARD & INBOARD AFT. REPAIRED SEAT TRACK IAW ER & EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FORWARD SEAT TRACK FASTENER HOLES CRACKED AT BS 727B, RBL 24.75, OUTBOARD FORWARD, OUTBOARD AFT, INBOARD FORWARD & INBOARD AFT. REPAIRED SEAT TRACK IAW ER & EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FORWARD SEAT TRACK FASTENER HOLES CRACKED AT BS 727B, LBL 24.75, OUTBOARD FORWARD, OUTBOARD AFT, INBOARD FORWARD & INBOARD AFT. REPAIRED SEAT TRACK PER ER & EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FORWARD SEAT TRACK FASTENER HOLES CRACKED AT BS 727B, RBL 45.5, OTBD FWD, OTBD AFT, INBD FWD & INBD AFT. REPAIRED SEAT TRACK IAW ER & EA.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,444 hrs · 17,165 cycles
LEFT HORIZONTAL STABILIZER INTERIOR CRACKED RIB AT STATION 92.70, 20" AFT FROM THE FWD LOWER SPAR CHORD, AT THE LOWER RADIUS INBD SIDE OF RIB. REPAIRED RIB IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 35,443 hrs · 17,165 cycles
FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA & ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FUSELAGE FRAME CRACKED AT BS 727B, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
RIGHT NR 3 FLIGHT DECK WINDOW FRAME CRACKED IN 2ND FASTENER HOLE FROM BOTTOM OF E - F POST. REPAIRED FRAME IAW SAM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,444 hrs · 17,165 cycles
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.