# N14816: 1985 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2006-07-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 5, 2006 - Exported to: Lebanon - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49370 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 18, 1985 - Certificate issued: January 26, 2001 - Last registry action: January 20, 2004 - Mode S code: A0C302 - Owner when cancelled: [Pacific Aircorp 49370 Inc](https://openairdocs.org/faa-owner/PACIFIC%20AIRCORP%2049370%20INC) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14816 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14816 - Page: https://openairdocs.org/deregistered/N14816-2006-07-05 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (78, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P9RA20050079](https://openairdocs.org/sdr/P9RA20050079), May 13, 2005: GIRT BAR. DIRTY. SFB GATE ITEM P1, L2 DOOR WILL NOT DISARM. CLEANED AND LUBRICATED GIRT BAR IAW MM. OPERATIONAL CHECKED NORMAL. - [SDR P9RA20040058](https://openairdocs.org/sdr/P9RA20040058), Dec 23, 2004: LIGHT. INOPERATIVE. A/C IN SYR, PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. - [SDR P9RA](https://openairdocs.org/sdr/P9RA), Dec 23, 2004: LIGHT. INOPERATIVE. A/C IN SYR. PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. - [SDR P9RA20040047](https://openairdocs.org/sdr/P9RA20040047), Oct 12, 2004: POWER SUPPLY. INOPERATIVE. AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM. - [SDR P9RA20040046](https://openairdocs.org/sdr/P9RA20040046), Oct 12, 2004: POWER SUPPLY. INOPERATIVE. AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHTS INOPERATIVE AT ROW 26. REMOVED AND REPLACED POWER SUPPLY IAW MM. - [SDR P9RA20040045](https://openairdocs.org/sdr/P9RA20040045), Sep 29, 2004: BATTERY. WEAK. AIRCRAFT IN MAINTENANCE, SYR, 4 INTERIOR EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERIES IN 4 SEPARATE POWER SUPPLIES IAW MM. - [SDR P9RA20040023](https://openairdocs.org/sdr/P9RA20040023), Jul 29, 2004: PROXIMITY SWITCH. STICKING. IB FLIGHT, APPROXIMATELY 10 MINUTES BEFORE LANDING, TAIL CONE ANNUNCIATOR ILLUMINATED AND REMAINED ON. QRH PROCEDURE FOLLOWED. NO EMERGENCY DECLARED. UNEVENTFUL - [SDR P9RA20040020](https://openairdocs.org/sdr/P9RA20040020), Jul 15, 2004: CHARGER. INOPERATIVE. IN INSPECTION, VARIOUS EMERGENCY EXIT LIGHTS OUT OVERHEAD. REMOVED AND REPLACED 3 BATTERY CHARGERS SERIAL NUMBERS 5227 15955 21872 AND AND 4 EMERGENCY BATTERIES - [SDR P9RA20040014](https://openairdocs.org/sdr/P9RA20040014), May 31, 2004: SLIDE. OUT OF POSITION. AT GATE IN CZM, THE L1 DOOR SLIDE FELL OUT OF ITS COVER. REINSTALLED L1 DOOR SLIDE COVER. - [SDR CALA0300280](https://openairdocs.org/sdr/CALA0300280), Jun 1, 2003: COMPRESSOR. FAILED. THE AIRFRAME SHUDDERED SLIGHTLY AND WAS ACCOMPANIED BY AN AUDIBLE BOOM AFTER TAKEOFF FROM IAH AT ABOUT 3,000 FEET. THE NR 1 ENGINE SUBSEQUENTLY AUTO SHUTDOWN. T - [SDR CALA0300169](https://openairdocs.org/sdr/CALA0300169), Apr 5, 2003: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 1418, L2L TO L2R. REMOVED AND REPLACED BELTFRAME IAW SRM 51-30-05. - [SDR CALA0100431](https://openairdocs.org/sdr/CALA0100431), Apr 29, 2001: CHARGER. INOPERATIVE. EMERGENCY LIGHTS AT REAR GALLEY DOOR AND TAIL CONE DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY VASE PER MM 33-53-00 PG 407. - [SDR CALA0001870](https://openairdocs.org/sdr/CALA0001870), Dec 7, 2000: SKIN. DENTED. INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED AT CENTER OF DOOR 15 INCHES FROM FORWARD EDGE. THE DENTED AREA WAS REMOVED AND DOUBLER AND FILLER WERE INSTALL - [SDR CALA0001851](https://openairdocs.org/sdr/CALA0001851), Dec 2, 2000: DOUBLER. DAMAGED. INSPECTION FOUND LT ELEVATOR TIP TRAILING EDGE DOUBLER DAMAGED. THE DOUBLER WAS REPLACED IAW SRM 51-10-2 AND 51-30-8. - [SDR CALA0001850](https://openairdocs.org/sdr/CALA0001850), Dec 2, 2000: DOUBLER. DAMAGED. INSPECTION FOUND LT ELEVATOR TIP TRAILING EDGE DOUBLER DAMAGED. THE DOUBLER WAS REPLACED IAW SRM 51-10-2 AND 51-30-8. - [SDR CALA0001841](https://openairdocs.org/sdr/CALA0001841), Nov 29, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED TWENTY INCHES BELOW LEFT PITOT PROBE AT FS 69.5. THE DENT WAS WORKED OUT TO ORIGINAL CONTOUR WITH NO CRACKS NOTED PER HFEC - [SDR CALA0001840](https://openairdocs.org/sdr/CALA0001840), Nov 28, 2000: CASTING. CRACKED. INSPECTION FOUND LT WING TIP LEADING EDGE CASTING CRACKED WITH POPPED RIVETS AND GOUGES. THE CASTING PANEL WAS REMOVED AND A NEW CASTING PANEL WAS INSTALLED IAW - [SDR CALA0001839](https://openairdocs.org/sdr/CALA0001839), Nov 28, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT PIT LT CARGO TRACK CORRODED. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-3, 51-30-1, AND 51-30-5. - [SDR CALA0001838](https://openairdocs.org/sdr/CALA0001838), Nov 28, 2000: SKIN. CORRODED. INSPECTION FOUND AFT CARGO DOOR INNER SKIN CORRODED AROUND RIVET NUTS. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 52-05, FIGURE 7. - [SDR CALA0001836](https://openairdocs.org/sdr/CALA0001836), Nov 24, 2000: FLOOR SUPPORT. BROKEN. INSPECTION FOUND FORWARD CARGO COMPARTMENT LT FLOORBEAM SUPPORT BROKEN AT FS 294. THE FLOORBEAM SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-3 - [SDR CALA0001817](https://openairdocs.org/sdr/CALA0001817), Nov 22, 2000: SUPPORT BRACKET. CORRODED. INSPECTION FOUND AFT CARGO PIT LT VERTICAL SUPPORT TO FLOOR TRANSITION PANEL CORRODED AT STA 1155 - 1212. THE VERTICAL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS - [SDR CALA0001816](https://openairdocs.org/sdr/CALA0001816), Nov 21, 2000: ANGLE. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN FORWARD CARGO DOOR SEAL FLANGE OPEN LOCK ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4 - [SDR CALA0001814](https://openairdocs.org/sdr/CALA0001814), Nov 20, 2000: FITTING. DENTED. INSPECTION FOUND LT WING NR 5 SLAT END FITTING DENTED. THE SLAT END FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4 AND 51-10-3. - [SDR CALA0001813](https://openairdocs.org/sdr/CALA0001813), Nov 20, 2000: STRAP. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB FORWARD TORQUE BOX LINER RETAINING STRAP CORRODED AND WORN AT STA 370. THE STRAP WAS REMOVED AND A NEW STRA - [SDR CALA0001812](https://openairdocs.org/sdr/CALA0001812), Nov 20, 2000: WEB. CORRODED. INSPECTION FOUND CUSP WEB DOUBLER CORRODED AT STA 207-218, L18L. A NEW DOUBLER WAS INSTALLED IAW SRM 53-01-1, 51-10-3, AND 51-30-5. - [SDR CALA0001810](https://openairdocs.org/sdr/CALA0001810), Nov 20, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT STA 522 - 786. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, A - [SDR CALA0001809](https://openairdocs.org/sdr/CALA0001809), Nov 20, 2000: STIFFENER. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN APB VERTICAL STIFFENER AT BL 0 ABOVE AFT ENTRANCE DOOR AT UPPER CORNER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS I - [SDR CALA0001807](https://openairdocs.org/sdr/CALA0001807), Nov 20, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT RT CARGO TIE DOWN TRACK CORRODED AT STA 218 - 370. THE TIE DOWN TRACK WAS REMOVED AND A NEW TIE DOWN TRACK WAS INSTAL - [SDR CALA0001805](https://openairdocs.org/sdr/CALA0001805), Nov 19, 2000: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK AND BEND IN LT HORIZONTAL STABILIZER TIP O/B LOWER AFT CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-11-0, 51-30-2, A - [SDR CALA0001804](https://openairdocs.org/sdr/CALA0001804), Nov 19, 2000: FRAME. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FRAME FOR LEFT VENTRAL STAIRS SIDEWALL PANEL. THE SIDEWALL SUPPORT WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-1 - [SDR CALA0001803](https://openairdocs.org/sdr/CALA0001803), Nov 19, 2000: DOUBLER. BENT. INSPECTION FOUND LEFT AFT NLG DOOR DOUBLER BENT AND SEPARATED AT AFT LOWER SECTION. THE DAMAGED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-3 - [SDR CALA0001802](https://openairdocs.org/sdr/CALA0001802), Nov 19, 2000: SKIN. CORRODED. INSPECTION FOUND MID CARGO DOOR INNER SKIN CORRODED AROUND RIVET NUTS. THE RIVET NUTS WERE REMOVED. A DOUBLER AND RIVET NUTS WERE INSTALLED IAW SRM 51-30-1, 52- - [SDR CALA0001801](https://openairdocs.org/sdr/CALA0001801), Nov 18, 2000: SKIN. GOUGED. INSPECTION FOUND RIGHT WING FLAP T/E PANEL 1613 SKIN GOUGED AND PITTED. THE SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 57-50-14. - [SDR CALA0001800](https://openairdocs.org/sdr/CALA0001800), Nov 17, 2000: CHANNEL. TORN. INSPECTION FOUND AFT EMERGENCY EXIT RAMP UPPER LEFT RAIL CHANNEL EDGE TORN AT FS 1474 WITH A LARGE DENT 20 INCHES AFT. THE TORN EDGE WAS BLENDED OUT AND REPAIR - [SDR CALA0001797](https://openairdocs.org/sdr/CALA0001797), Nov 17, 2000: STOP. CHAFED. INSPECTION FOUND MID CARGO DOOR STOP NR 12 CHAFED. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819. - [SDR CALA0001796](https://openairdocs.org/sdr/CALA0001796), Nov 17, 2000: RIB. GOUGED. INSPECTION FOUND LEFT WING O/B EDGE OF RIB GOUGED AT NR 15 SLAT TRACK CUTOUT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-30-2, 51-30-6, 51-30-4, - [SDR CALA0001795](https://openairdocs.org/sdr/CALA0001795), Nov 17, 2000: SKIN. GOUGED. INSPECTION FOUND LT FORWARD NLG DOOR SKIN GOUGED AT FORWARD UPPER CORNER. THE GOUGED AREA WAS REMOVED IAW SRM 52-01, FIGURE 1. REPAIR PARTS WERE INSTALLED IAW S - [SDR CALA0001794](https://openairdocs.org/sdr/CALA0001794), Nov 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, RBL 12 - RBL 42. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10- - [SDR CALA0001793](https://openairdocs.org/sdr/CALA0001793), Nov 17, 2000: STRUCTURE. CORRODED. INSPECTION FOUND SUB FLOOR WEB CORRODED AT STA 165 - 200, LBL 52. THE SUB FLOOR WAS REMOVED AND A NEW SUB FLOOR WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-05, FI - [SDR CALA0001792](https://openairdocs.org/sdr/CALA0001792), Nov 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED ON LOWER SURFACE AT STA 218 - 256, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 5 - [SDR CALA0001791](https://openairdocs.org/sdr/CALA0001791), Nov 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, RBL 44 AND AT STA 148 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51- - [SDR CALA0001790](https://openairdocs.org/sdr/CALA0001790), Nov 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, RBL 9 - RBL 45 AND AT LBL 5 - RBL 5. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-10 - [SDR CALA0001789](https://openairdocs.org/sdr/CALA0001789), Nov 17, 2000: SKIN. GOUGED. INSPECTION FOUND RT MLG FORWARD DOOR SKIN GOUGED AT FORWARD UPPER CORNER. THE GOUGED AREA WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 52-01, FIGURE 1, 5 - [SDR CALA0001788](https://openairdocs.org/sdr/CALA0001788), Nov 17, 2000: STOP. CHAFED. INSPECTION FOUND MID CARGO DOOR STOPS NR 3, 4, 6 & 8 CHAFED. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-02819. - [SDR CALA0001787](https://openairdocs.org/sdr/CALA0001787), Nov 17, 2000: FITTING. CORRODED. INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED AT STA 216, RBL 55. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, - [SDR CALA0001786](https://openairdocs.org/sdr/CALA0001786), Nov 17, 2000: FITTING. CORRODED. INSPECTION FOUND RT FRAME TO FLOOR FITTING CORRODED AT STA 579, LONGERON 18R. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-3, 51-30-5, - [SDR CALA0001785](https://openairdocs.org/sdr/CALA0001785), Nov 17, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1185, LONGERON 18L. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5331-2-A0800. - [SDR CALA0001777](https://openairdocs.org/sdr/CALA0001777), Nov 16, 2000: ANGLE. CORRODED. INSPECTION FOUND FLOOR SUPPORT ANGLE AND PLATE CORRODED AT FS 148 - 200, RBL 55. THE ANGLE AND PLATE WERE REMOVED AND A NEW ANGLE AND PLATE WERE INSTALLED IAW S - [SDR CALA0001776](https://openairdocs.org/sdr/CALA0001776), Nov 16, 2000: WEB. CRACKED. INSPECTION FOUND TWO, 1 INCH CRACKS IN E&E COMPARTMENT CABIN PRESSURE WEB AT STA 190, RBL 48. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, 51-30-3, AND 51-30-2 - [SDR CALA0001773](https://openairdocs.org/sdr/CALA0001773), Nov 15, 2000: SKIN. GOUGED. INSPECTION FOUND RT WING NR 4 FLAP O/B TRAILING EDGE SKIN GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2. All 78: https://openairdocs.org/deregistered/N14816-2006-07-05/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DEN93FA047](https://openairdocs.org/ntsb/DEN93FA047), Apr 26, 1993: Mcdonnell Douglas DC-9-82 (N14816), Denver, CO, substantial damage. Probable cause: AN INFLIGHT ENCOUNTERWITH A MICROBURST AT AN ALTITUDE INSUFFICIENT TO EFFECT RECOVERY. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19970314009129I](https://openairdocs.org/incident/19970314009129I), Mar 14, 1997: Doug DC982 (N14816), El Paso, TX. Narrative: on March 14, 1997, continenetal airlines flight 148, a MD-80 was enroute from los angeles, CA (lax) to houston, TX. Approximately one hour out of… - [Accident 19930426010599A](https://openairdocs.org/incident/19930426010599A), Apr 26, 1993: Doug DC982 (N14816), Denver, CO, Substantial damage. Indicates wind shear on short final. High sink. Power and rotation not effective. Struck tail on hard landing. ## Other aircraft with N14816 - [Cancelled 1980-10-22](https://openairdocs.org/deregistered/N14816-1980-10-22): Bell 206B, S/N 848, built 1972. Exported to Ecuador. Owner: [Petroleum Helicopters Inc](https://openairdocs.org/faa-owner/PETROLEUM%20HELICOPTERS%20INC), [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.